EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

96
EXPERIMENTAL RESEARCH ON THE' BUCKLING BEHAVIOUR OF SLENDER PRESTRESSED CONCRETE COLUMNS by GYORGY LASZLO Diploma of Civil Engineering Jozsef Nador University Budapest A THESIS SUBMITTED IN PARTIAL FULFILMENT THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE IN ENGINEERING in the Department of CIVIL ENGINEERING We accept this thesis as conforming to the required standard THE UNIVERSITY OF BRITISH COLUMBIA April, 1966

Transcript of EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

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EXPERIMENTAL RESEARCH ON THE' BUCKLING BEHAVIOUR OF SLENDER PRESTRESSED

CONCRETE COLUMNS

by

GYORGY LASZLO

D i p l o m a of C i v i l E n g i n e e r i n g

J o z s e f Nador U n i v e r s i t y B u d a p e s t

A THESIS SUBMITTED IN PARTIAL FULFILMENT

THE REQUIREMENTS FOR THE DEGREE OF

MASTER OF SCIENCE IN ENGINEERING

i n t h e D e p a r t m e n t

of

C I V I L ENGINEERING

We a c c e p t t h i s t h e s i s as c o n f o r m i n g t o the

r e q u i r e d s t a n d a r d

THE UNIVERSITY OF BRIT I S H COLUMBIA

A p r i l , 1966

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I n p r e s e n t i n g t h i s t h e s i s i n p a r t i a l f u l f i l m e n t of

the r e q u i r e m e n t s f o r an advanced degree at the U n i v e r s i t y of

B r i t i s h Columbia, I agree t h a t the L i b r a r y s h a l l make i t f r e e l y

a v a i l a b l e f o r r e f e r e n c e and s t u d y t I f u r t h e r agree t h a t p e r ­

m i s s i o n f o r e x t e n s i v e c o p y i n g of t h i s t h e s i s f o r s c h o l a r l y

purposes may be granted by the Head of my Department or by

h i s r e p r e s e n t a t i v e s . I t i s understood t h a t ; c o p y i n g or p u b l i ­

c a t i o n of t h i s t h e s i s f o r f i n a n c i a l g a i n s h a l l , not be a l l o w e d

w i t h o u t my w r i t t e n p e r m i s s i o n *

Department o f C i v i l E n g i n e e r i n g

The U n i v e r s i t y of B r i t i s h Columbia, Vancouver 8 5 Canada

Date A p r i l , 1966.

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i .

ACKNOWLEDGMENTS

T h i s t e s t was c o n d u c t e d u n d e r t h e s u p e r v i s i o n o f P r o f e s s o r

Samuel L. L i p s o n , D e p a r t m e n t of C i v i l E n g i n e e r i n g . The a b l e

a s s i s t a n c e o f t h e s t a f f of G r a y b a r P r e c a s t L i m i t e d i n t h e

f a b r i c a t i o n o f t h e s p e c i m e n s , and of t h e s t a f f of t h e C i v i l

E n g i n e e r i n g D e p a r t m e n t i n t h e t e s t i n g , i s g r e a t l y a p p r e c i a t e d .

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i i .

ABSTRACT

T h i r t y f u l l s c a l e p r e s t r e s s e d c o n c r e t e s t r u t s a l l h a v i n g a

s l e n d e r n e s s r a t i o o f L/D = 40 were t e s t e d w i t h t h r e e d i f f e r e n t

e c c e n t r i c i t i e s . S t r e s s - s t r a i n c u r v e s o f t h e c o r r e s p o n d i n g

t e s t c y l i n d e r s were e s t a b l i s h e d and t h e Young's M o d u l i e v a l u a t e d .

The s p e c i m e n s were f a b r i c a t e d w i t h d i f f e r e n t p e r c e n t a g e s o f

p r e s t r e s s i n g s t e e l r a n g i n g f r o m ,0.23 t o 1.20$. The i n i t i a l

p r e s t r e s s i n g f o r c e s were s e t t o o b t a i n a f i n a l p r e s t r e s s of

140,000 p s i i n a l l s p e c i m e n s . The d i m e n s i o n s o f t h e s t r u t s ,

and t h e q u a l i t y and m a n u f a c t u r i n g p r o c e s s o f t h e c o n c r e t e , were

k e p t c o n s t a n t . S p e c i a l a d j u s t a b l e s u p p o r t i n g d e v i c e s s i m u l a t e d

i d e a l h i n g e d c o n d i t i o n s . The s t r u t s were t e s t e d t o t h e i r

u l t i m a t e c a p a c i t y and t h e i r c r i t i c a l b u c k l i n g l o a d s were

e v a l u a t e d .

The t e s t s p r o v e d t h a t , p r o v i d e d t h e column i s made of h i g h

q u a l i t y c o n c r e t e , t h e c r i t i c a l l o a d v a l u e s can be o b t a i n e d by

u s i n g B u l e r ' s f u n d a m e n t a l f o r m u l a , and t h e s e v a l u e s a r e

i n d e p e n d e n t o f t h e amount o f p r e s t r e s s i n g . F o r e c c e n t r i c a l l y

l o a d e d s t r u t s maximum s t r e s s e s f r o m a m o d i f i e d s e c a n t f o r m u l a ,

i n c o r p o r a t i n g e f f e c t o f p r e s t r e s s i n g , were compared w i t h t h o s e

c a l c u l a t e d on b a s i s o f o b s e r v e d d e f l e c t i o n s .

A c c o r d i n g t o t h e t e s t r e s u l t s t h e s e c a n t modulus- c o r r e s p o n d ­

i n g t o t h e a v e r a g e c o m p r e s s i v e s t r e s s s h o u l d be u s e d i n E u l e r ' s

f o r m u l a .

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i i i .

TABLE 1 OF CONTENTS

PAGE

C h a p t e r I . - I n t r o d u c t i o n , . . 1

C h a p t e r I I . - O b j e c t and Scope of T e s t s 4

C h a p t e r I I I . - D e s c r i p t i o n of t h e S p e c i m e n s ............ 7

C h a p t e r I V . - P r e p a r a t i o n o f t h e S p e c i m e n s

1. M i x i n g of C o n c r e t e 14

2. Bed E q u i p m e n t and S t r e s s i n g 14

3. P l a c i n g the C o n c r e t e .................... 16

4. C u r i n g and D e s t r e s s i n g of t h e S p e c i m e n s . . 18

5. S h i p m e n t o f the S p e c i m e n s 18

Cha p t e r ' V.- T e s t P r o c e d u r e

1 . T e s t i n g M a c h i n e 20

, 2. D e f l e c t i o n Measurement .................. 20

3. Mechanism o f the S t r u t S u p p o r t 21

4. S p e c i a l T e s t s ........................... 24

5. C y l i n d e r T e s t s 27

C h a p t e r V I . - T e s t R e s u l t s

1 . G e n e r a l 28

2. T a b u l a t e d O b s e r v a t i o n s ........ ......... . 32

3. T a b u l a t e d C a l c u l a t i o n s . .

A. C r i t i c a l L o a d s . . . . . . . . . . . . . . 43

B. S t r e s s e s . . . . . . . . . . . . . . . 60

4. C a l c u l a t i o n o f the M o d u l i ............... 61

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i v .

•PAGE

C h a p t e r V I I . - D i s c u s s i o n of T e s t R e s u l t s

1 . I n f l u e n c e of S t e e l R a t i o on

t h e C r i t i c a l Load 69

2. A p p l i c a b i l i t y o f the S o u t h w e l l M e t hod... 70

3. The M o d u l u s t o be Used. 71

4. U l t i m a t e Load C a r r y i n g C a p a c i t y 75

C h a p t e r V I I I . - C o n c l u s i o n s 80

R e f e r e n c e s . 81

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L I S T OF TABLES

TABLE .PAGE

I . - Types of S p e c i m e n s 6

l l . - M a n u f a c t u r i n g D a t a of t h e S p e c i m e n s . . . . . . . 9

I I I . - T e s t R e s u l t s 33

I V . - C o m p a r i s o n of S t r e s s e s O b t a i n e d f r o m the

T e s t R e s u l t s w i t h Those Computed by

B r e c k e n r i d g e ' s M o d i f i e d S e c a n t F o r m u l a . 62

V. - C o m p a r i s o n of D i f f e r e n t M o d u l i 68

V I , - R e d u c t i o n F a c t o r s ' f o r S t r u t s w i t h Z e r o

E c c e n t r i c i t y . , , , . . . 78

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L I S T OF FIGURES

FIGURE PAGE

1 . D e t a i l s o f S p e c i m e n s 8

2. D e t a i l s of t h e End P l a t e and the

F a s t e n i n g D e v i c e 12

3. D e t a i l s o f t h e S t r e s s i n g E q u i p m e n t 15

4. S c h e m a t i c D e s c r i p t i o n o f t h e S t r e s s i n g P r o c e d u r e 17

5. C r i t i c a l L o a d s f o r S p e c i m e n s w i t h Z e r o

and 0.3 i n . E c c e n t r i c i t i e s 29

6. C r i t i c a l L o a d s f o r S p e c i m e n s w i t h Z e r o

E c c e n t r i c i t y O n l y 30

7. C r i t i c a l L oads f o r S p e c i m e n s w i t h 0.3 i n .

' E c c e n t r i c i t y O n l y 31

8/1-8/4. L o a d - d e f l e c t i o n C u r v e s of S p e c i m e n s w i t h

1.5 i n . E c c e n t r i c i t i e s 37-40

9. L o a d - d e f l e c t i o n C u r v e f o r S p e c i m e n No. 29

T e s t e d t o D e s t r u c t i o n 41

10. The Two Types o f Load E c c e n t r i c i t i e s Used 47

1 l / a - 1 l / c . T y p i c a l S o u t h w e l l P l o t s 48-50

1 l / d - 1 l / e . T y p i c a l S o u t h w e l l P l o t s 52-53

1 l / f - 1 l / i . T y p i c a l S o u t h w e l l P l o t s 55-58

12. V a r i a t i o n o f R a t i o P /P w i t h S t e e l u c r

C o n t e n t 59

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v i i .

FIGURE PAGE

13/a— 1 3/"b • C u r v e s of t h e S e c a n t F o r m u l a P l o t t e d

f o r t h e S p e c i m e n s "'"765^64

14/a-14/b. T y p i c a l S t r e s s - s ' t r a i n C u r v e s f o r

C y l i n d e r s . ' : 66-67

15. C o n v e r t e d C r i t i c a l L oads V e r s u s V a l u e s

of a 72

16. C o m p a r i s o n of E u l e r C u r v e w i t h the

C o n v e r t e d C r i t i c a l Loads 74

17. C o m p a r i s o n o f Commonly Used C u r v e s o f

Mo d u l u s w i t h T e s t R e s u l t s 76

18. U l t i m a t e Load of S t r u t s w i t h 1.5 i n .

E c c e n t r i c i t y V e r s u s S t e e l R a t i o . . . . . . 79

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\ i i i .

L I S T OF PHOTOGRAPHS

PHOTO PAGE

1. The F a s t e n i n g D e v i c e f o r t h e

A d j u s t a b l e P l a t e . 23

2. ' The S t r u t D u r i n g T e s t i n g . 25

3. B u c k l e d S t r u t w i t h Low P r e s t r e s s 36

4. T e n s i o n F a i l u r e of S p e c i m e n No. 2 9 . . . . . . 42

5. C o m p r e s s i o n F a i l u r e o f S p e c i m e n No. 22.. 44

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SYMBOLS

( i n . ) O b s e r v e d I n i t i a l C u r v a t u r e

( i n . ) I n i t i a l E c c e n t r i c i t y (due t o t h e co m b i n e d

e f f e c t o f the : i n i t i a l c u r v a t u r e and t h e

l o a d e c c e n t r i c i t y ) 2

A ( i n . ) G r o s s A r e a of 'the C o n c r e t e

a o a1

•c A„ ( i n . * ) A c t u a l A r e a o f t h e S t r a n d s s

c ( i n . ) D e p t h o f N e u t r a l A x i s f r o m E x t r e m e Compress­

i o n F i b r e s

C q ( i n . / i n . ) C r e e p C o e f f i c i e n t

C ( i n . / i n . ) S h r i n k a g e C o e f f i c i e n t s

D ( i n . ) D i m e n s i o n o f t h e S t r u t i n t h e D i r e c t i o n o f

B u c k l i n g

e ( i n . ) Load E c c e n t r i c i t y

E ( k s i ) M o d u l u s o f E l a s t i c i t y o f t h e C o n c r e t e

E' ( k s i ) A r b i t r a r y M o d ulus o f E l a s t i c i t y s e t a t

3,320 k s i

E^ ( k s i ) M o d u l u s o f e l a s t i c i t y O b t a i n e d by' the B e n d i n g

T e s t o f S i x S p e c i m e n s E ( k s i ) M o d u l u s o f E l a s t i c i t y as D e t e r m i n e d by Pauw's P

F o r m u l a

E^ ( k s i ) M o d u l u s o f E l a s t i c i t y o f t h e T e s t C y l i n d e r a t

t h e A n t i c i p a t e d A v e r a g e C o m p r e s s i v e S t r e s s

E, . ( k s i ) T a n g e n t Modulus of E l a s t i c i t y a t Z e r o S t r e s s "C 1

E ( k s i ) M o d u l u s o f E l a s t i c i t y o f t h e S t e e l s

f ( p s i ) F i n a l C o n c r e t e S t r e s s a f t e r L o s s e s

f ^ ( p s i ) U l t i m a t e S t r e n g t h o f the T e s t C y l i n d e r

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f " c ( p s i ) C o m p r e s s i v e S t r e n g t h of C o n c r e t e i n F l e x u r e

f 1 ( k s i ) L o s s i n P r e s t r e s s

f . SI

( k s i ) I n i t i a l P r e s t r e s s o f t h e S t e e l

f s o

( k s i ) P i n a l P r e s t r e s s a f t e r L o s s e s

f s u

( k s i ) S t r e s s i n t h e S t e e l a t Load P*

F so

( k i p ) S t r e s s i n g F o r c e C o r r e s p o n d i n g t o f = 140,000 p s i so e

F s u

( k i p ) S t r e s s i n g F o r c e C o r r e s p o n d i n g t o f

I ( i n . 4 ) Moment of I n e r t i a o f t h e S t r u t

L ( i n . ) L e n g t h o f t h e S t r u t ( b e t w e e n o u t s i d e f a c e s o f t h e Embedded P l a t e s )

n M o d u l a r R a t i o o f S t e e l t o C o n c r e t e

P R a t i o o f S t e e l A r e a t o C o n c r e t e A r e a

P ( k i p ) A x i a l Load on t h e S t r u t

P' ( k i p ) T e s t Load a t t h e L a s t R e a d i n g I n c r e m e n t b e f o r e B u c k l i n g O c c u r r e d

P c r

( k i p ) C r i t i c a l I^oad D e t e r m i n e d f r o m t h e S o u t h w e l l P c r P l o t s

P 0

( k i p ) S h o r t Column S t r e n g t h = . 8 5 f " ( A c ~ A g )

R R e d u c t i o n F a c t o r P +F /P u su 0

t ( i n . ) W i d t h o f t h e S t r u t i n the N a r r o w D i r e c t i o n

T ( d a y ) E l a p s e d Time between M a n u f a c t u r e and T e s t i n g

w c

( l b . / c u . f t . ) U n i t W e i g h t of C o n c r e t e

X ( i n . ) D i s t a n c e b e t w e e n t h e E x t r e m e F i b r e and t h e C e n t r o i d o f t h e S e c t i o n

oC. R a t i o o f A p p l i e d Load t o C r i t i c a l L o ad oC* R a t i o o f E ' / E t

(3 ( l / i a . ) C r i t i c a l C u r v a t u r e & ( i n . ) O b s e r v e d L a t e r a l D e f l e c t i o n o f t h e M i d - P o i n t

of t h e S t r u t

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x i .

C r i t i c a l S t r a i n i n C o n c r e t e a t M i d - P o i n t

due t o t h e Combined E f f e c t of P c"and P su u

A v e r a g e C o n c r e t e S t r e s s a t Load P' I n c o r p o r a t ­

i n g t h e E f f e c t o f S t r e s s L o s s e s

Maximum C o m p r e s s i o n S t r e s s a t Load P' ,

Maximum T e n s i o n S t r e s s a t Load P'

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I. INTRODUCTION

W i t h t h e r e c e n t t r e m endous g r o w t h i n t h e use of p r e s t r e s s e d

c o n c r e t e s t r u c t u r e s t h e d e s i g n e r s a r e t r y i n g t o expand t h e a r e a

o f a p p l i c a t i o n o f t h i s r e l a t i v e l y new m a t e r i a l . I n t h i s way

t h e u se of s l e n d e r p r e s t r e s s e d columns i s g r a d u a l l y i n c r e a s i n g .

I t has become a p p a r e n t t h a t t h e m a n u f a c t u r e o f s l e n d e r columns

by p r e s t r e s s i n g o f f e r s many a d v a n t a g e s . When b u i l d i n g e l e m e n t s

a r e p r e f a b r i c a t e d t h e p r o b l e m o f t r a n s p o r t a t i o n becomes p r e ­

d o m i n a n t . I n t h e c a s e o f l a r g e s l e n d e r u n i t s , r e g a r d l e s s o f

t h e i r f i n a l u s e , i t i s o f t e n a d v i s a b l e t o d e s i g n i n p r e s t r e s s e d

c o n c r e t e t o a v o i d c r a c k i n g d u r i n g h a n d l i n g and t r a n s p o r t a t i o n .

A l s o , t h e r e i s an i n c r e a s i n g need f o r p r e s t r e s s e d b e a r i n g w a l l

u n i t s whose s l e n d e r n e s s i s d i c t a t e d by a r c h i t e c t u r a l f e a t u r e s .

E x p e r i e n c e has p r o v e n t h a t t h e s a v i n g i n t r a n s p o r t a t i o n c o s t s

due t o b e t t e r f l e x u r a l p r o p e r t i e s , o f f s e t s t h e l o s s i n com­

p r e s s i v e c a p a c i t y . A l s o , t h e r e i s o f t e n a need f o r c r a c k - f r e e

c o n c r e t e e l e m e n t s .

I t i s b e l i e v e d t h a t t h e r e c o g n i t i o n o f t h e s e a d v a n t a g e s

has l e d i n v e s t i g a t o r s t o t u r n t h e i r i n t e r e s t t o w a r d s t h e

s t u d y of the b e h a v i o u r o f p r e s t r e s s e d c o n c r e t e c o l u m n s .

A s e r i e s o f s t u d i e s , i n v e s t i g a t i n g t h e b e h a v i o u r o f p r e -

s t r e s s e d c o l u m n s , was s t a r t e d by R. A. B r e c k e n r i d g e . I n

h i s e x p e r i m e n t a l r e s e a r c h , p u b l i s h e d i n 1953, B r e c k e n r i d g e

p r o v e d t h a t a c o n c e n t r i c a l l y p l a c e d t e n d o n o r p r e t e n s i o n i n g

w i r e has no e f f e c t on t h e c r i t i c a l s u p e r i m p o s e d l o a d w h i c h

t h e c o l u m n s w i l l c a r r y , as l o n g as t h e p r e s t r e s s does n o t

e x c e e d t h e d i f f e r e n c e b e t w e e n t h e c r i t i c a l l o a d and t h e

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2.

u l t i m a t e c o m p r e s s i v e s t r e n g t h of the c o n c r e t e .

He a l s o i n c o r p o r a t e d the l o s s of p r e s t r e s s due t o s u p e r ­

i m p o s e d a x i a l l o a d i n t o a g e n e r a l i z e d e q u a t i o n . F i n a l l y he

m o d i f i e d t h e s e c a n t f o r m u l a i n o r d e r t o compute t h e s t r e s s e s

i n an a x i a l l y p r e s t r e s s e d and e c c e n t r i c a l l y l o a d e d c o l u m n .

To v e r i f y t h e s e e q u a t i o n s he t e s t e d 71 columns of f i v e t y p e s

h a v i n g s l e n d e r n e s s r a t i o s r a n g i n g "between 84 and 155.

O t h e r s t u d i e s have a l s o been p u b l i s h e d s h o w i n g t h a t t h e

u l t i m a t e c a p a c i t y of an e c c e n t r i c a l l y l o a d e d p r e s t r e s s e d c o n ­

c r e t e c o l u m n does depend on t h e p e r c e n t a g e o f t h e p r e s t r e s s i n g

s t e e l . Some a u t h o r s , f o r e x a m p l e , • P a u l Zung-Teh Z i a i n h i s 20

" U l t i m a t e S t r e n g t h o f S l e n d e r P r e s t r e s s e d C o n c r e t e Columns" p r e s e n t e d g r a p h s s h o w i n g a r e l a t i o n s h i p b etween p e r c e n t a g e of

s t e e l and u l t i m a t e c a p a c i t y of a p r e s t r e s s e d c o n c r e t e s t r u t .

,The maximum s l e n d e r n e s s r a t i o i n h i s e x p e r i m e n t s was L/D = 35.

The a u t h o r s t a t e d t h a t optimum r e s u l t s a r e o b t a i n e d u s i n g 0.5$

to 1.0$ s t e e l . I n 1956, A. M. O z e l l and A. M. J e r n i g a n 1 0

i n v e s t i g a t e d the n e c e s s a r y p r e s t r e s s i n g i n ter m s of the s l e n d e r ­

n e s s r a t i o . C o m p u t a t i o n method f o r p r e s t r e s s e d columns i s

g i v e n 'by t h e c o m p r e h e n s i v e e x p e r i m e n t a l and t h e o r e t i c a l s t u d y 9

of T. Y. L i n and R. I t a y a p u b l i s h e d i n 1957. R e c e n t l y P r o f . 4

A. E f s e n d e v e l o p e d methods o f c a l c u l a t i o n of e c c e n t r i c a l l y l o a d e d p r e s t r e s s e d c o n c r e t e c o l u m n s , (196 3 ) - A. S. H a l l a l s o

5

' c o n c l u d e d i n h i s e x p e r i m e n t a l r e s e a r c h t h a t t h e l o a d c a r r y i n g

c a p a c i t y of t h e h i g h l y p r e s t r e s s e d c o n c r e t e c o l u m n h a v i n g a

l o a d e c c e n t r i c i t y of L/40 was i n c r e a s e d by 60 p e r c e n t , w hereas

" i n no i n s t a n c e was any b e n e f i c i a l e f f e c t g a i n e d "by a p r e s t r e s s

Page 16: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

' 2

l e s s t h a n 0.2 f ", ( 1 9 6 3 ) . Brown, K.I.. , i n h i s comprehen­

s i v e p a p e r a b o u t t h e b e h a v i o u r o f p r e s t r e s s e d c o n c r e t e c o l u m n s ,

p u b l i s h e d an i n e l a s t i c a n a l y t i c a l method t o c a l c u l a t e t h e

d e f l e c t i o n o f a s t r u t i n terms of t h e l o a d . He a l s o c o n c l u d e d

t h a t t h e amount o f p r e s t r e s s i n g does n o t i n f l u e n c e t h e s t a b i l ­

i t y of a s t r u t .

I n t h i s t h e s i s an a t t e m p t . i s made t o c o n t r i b u t e t o t h e

c l a r i f i c a t i o n o f t h e b u c k l i n g b e h a v i o u r of p r e s t r e s s e d c o n c r e t e

c o l u m n s .

The r e s e a r c h m a i n l y c o n c e n t r a t e d on i n v e s t i g a t i n g t h e

r e l a t i o n s h i p b e t ween t he E u l e r l o a d and t h e p e r c e n t a g e o f

s t e e l , and on e s t a b l i s h i n g t h e modulus t o be u s e d i n c a l c u l a t ­

i n g t h e E u l e r l o a d . Some columns were t e s t e d e c c e n t r i c a l l y i n

o r d e r t o s u p p o r t the v a l i d i t y of B r e c k e n r i d g e ' s m o d i f i e d s e c a n t

• f o r m u l a . A l l t e s t s were made on f u l l s c a l e models h a v i n g

i d e n t i c a l s l e n d e r n e s s r a t i o s of L/D = 40.

Page 17: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

II. OBJECT AND SCOPE OF TESTS

The pr imary o b j e c t i v e s of these t e s t s were to study the

f o l l o w i n g :

1) Whether there i s any r e l a t i o n s h i p between the E u l e r

load of a s l ender p r e s t r e s s e d concrete s t r u t and the

percentage of p r e s t r e s s i n g s t e e l .

2) Wheth er E u l e r ' s fundamental formula can be a p p l i e d i n

case of p r e s t r e s s e d s t r u t s .

3) ' Whether the b u c k l i n g load f o r a p r e s t r e s s e d s t r u t can

be p r e d i c t e d from the s t r e s s - s t r a i n curve of s tandard '

t e s t c y l i n d e r s .

In order to answer these quest ions t h i r t y ,(30) f u l l s c a l e

models were t e s t e d . It was dec ided to conf ine the scope of

the re sea r ch to one p a r t i c u l a r s lenderness r a t i o of L/D = 40,

and c e n t r a l p r e s t r e s s .

Wi th in the one va lue of s lenderness r a t i o the f o l l o w i n g

were kept constants

1) . Concrete s t reng th (designed f o r 6000 p s i ) .

2) F i n a l p r e s t r e s s i n the s trands (designed f o r

140,000 p s i ) .

3) Q u a l i t y of i n g r e d i e n t s i n order to ' ob ta in i d e n t i c a l

modulus.

4) Dimensions of the specimens.

and the f o l l o w i n g v a r i a b l e s were used:

1) S t e e l r a t i o (p = 0.23, 0.45, 0 . 6 , *0 .91, 1.20).

2) Load e c c e n t r i c i t y (e / t = 0,' 0. 1 •, 0 .5 ) .

Page 18: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

J »

The f i v e v a l u e s of s t e e l r a t i o p r o d u c e d p r e s t r e s s e s a f t e r

l o s s e s r a n g i n g f r o m 328 p s i t o 1680 p s i as shown i n T a b l e I .

The c r o s s s e c t i o n o f a l l t h e s p e c i m e n s was made r e c t a n g u l a r

r a t h e r t h a n s q u a r e . I n t h i s way t h e d i r e c t i o n o f t h e b u c k l i n g

c o u l d be p r e d i c t e d . T h i s a r r a n g e m e n t a l s o made t h e p o s i t i o n ­

i n g o f the l o a d and t h e . l a t e r a l d e f l e c t i o n measurement as

s i m p l e as p o s s i b l e .

S i n c e t h e p r i n c i p a l s c o p e o f t h e t e s t was. t o s t u d y b u c k l i n g

b e h a v i o u r , an a t t e m p t was made t o s i m u l a t e i d e a l h i n g e d c o n ­

d i t i o n s a t ' b o t h endso

None of t h e s p e c i m e n s had s t i r r u p r e i n f o r c e m e n t . A l t h o u g h 1 0

O z e l l and J e r n i g a n f o u n d i n t h e i r e x p e r i m e n t a l r e s e a r c h t h a t

t h e u l t i m a t e c a p a c i t y o f an e c c e n t r i c a l l y p r e s t r e s s e d s t r u t

h a v i n g s t i r r u p s i s g r e a t e r t h a n t h e one w i t h o u t s t i r r u p s , i t

was f e l t t h a t t h e use o f s t i r r u p s does n o t i n f l u e n c e t h e

b u c k l i n g c a p a c i t y o f c e n t r a l l y p r e s t r e s s e d s t r u t s .

To e s t a b l i s h t h e c o n c r e t e s t r e n g t h and Young's M o d u l u s o f

the s p e c i m e n a t t h e t i m e o f t e s t i n g , s i x 6" x 12" c y l i n d e r s

were e a s t u n d e r i d e n t i c a l c o n d i t i o n s w i t h t h e s p e c i m e n s - I t

was c o n t e m p l a t e d t o b r e a k two of each s e t a t t h e t i m e of de-

s t r e s s i n g and t h e o t h e r f o u r a t the t i m e o f t e s t i n g .

I t was d e c i d e d t o e s t a b l i s h t h e modulus a t t h e t i m e of

b u c k l i n g u s i n g t h e s t r e s s - s t r a i n c u r v e s o b t a i n e d f r o m t h e

c y l i n d e r s r a t h e r t h a n m e a s u r i n g t h e s t r a i n s on t h e s t r u t s

d u r i n g t e s t i n g .

Page 19: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

6.

ITEM

MUAA&E.R-

o r ' S P E C I M E N

S T E b L RATIO

p M

APPLIED INITIAL E X P E C T E D F I N A L STfce-vS IN PTISAN PS

FINAL cONCfc.

6 T R E S 6 S T R A N G ITEM

MUAA&E.R-

o r ' S P E C I M E N

S T E b L RATIO

p M lb . P 4 I .

1 6 0.23 9,038 328 1-5/16"

2 6 0.45 17,588 635 1 -7/1-6"

3 6 0. 60 23,577 140,000 840 1-1/2"

4 6 0.91 18,534 * ) . 1 ,275 2-7/16" 9 18,362

5 6 1 .20 25,454 ft) 1 , 680 2-1/2" I 25,154

* Applied \o the f i r s t s f r a n d

TABLE I . - TYPES OF SPECIMENS

Page 20: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

7.

I I I . DESCRIPTION OF THE SPECIMENS

The t e s t s t r u t s were m a n u f a c t u r e d i n the p l a n t o f G r a y b a r

P r e c a s t L i m i t e d , and s h i p p e d t o t h e U n i v e r s i t y , of B r i t i s h

C o l u m b i a a f t e r a l l s t r u t s were c a s t .

The t h i r t y s t r u t s were p r e p a r e d i n f i v e m a j o r g r o u p s ,

e a c h g r o u n c o n t a i n i n g s i x i d e n t i c a l s p e c i m e n s .

F i g u r e 1, shows t h e f i v e t y p e s o f specimen,- and T a b l e I

p r e s e n t s t h e b a s i c d a t a of the s p e c i m e n s u s e d .

The f o l l o w i n g c o n c r e t e mix d e s i g n was u s e d f o r a l l

s p e c i m e n s :

Cement (Type I I I , E l k B r a n d , H i g h - E a r l y ) 180 l b s . Sand 251 3/8" a g g r e g a t e 108 3/4" a g g r e g a t e 374 Water 77

990 l b s . p e r b a t c h

The c o n c r e t e s t r e n g t h was c o n t r o l l e d 'by s t a n d a r d 6" x 12"

c y l i n d e r s , s i x b e i n g t a k e n f r o m e ach day's c a s t . T h r o u g h o u t

t h e t e s t t h e c o n c r e t e m i x , t h e i n i t i a l p r e s t r e s s i n g f o r c e ,

t h e m i x i n g t i m e , and t h e v i b r a t i o n t i m e were k e p t c o n s t a n t .

An a t t e m p t was made t o m a i n t a i n u n i f o r m m a n u f a c t u r i n g p r o c e d ­

u r e f o r a l l s p e c i m e n s : t h e v a r i a t i o n s a r e shown i n T a b l e I I .

The i n i t i a l p r e s t r e s s was computed so as t o e x p e c t a f i n a l

p r e s t r e s s o f 140,000 p s i .

The f o l l o w i n g a s s u m p t i o n s were made t o p r e d i c t p r e s t r e s s

l o s s e s :

a) To compute e l a s t i c s h o r t e n i n g and c r e e p t h e modulus

of t h e c o n c r e t e was assumed t o be 5,550 k s i and f o r

Page 21: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

8.

L I & W T

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Page 22: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

1. | 3 . 4- 5 . (P. 7 . &. 9 . I I . I -2 . 1 3 . 14- | 5 . \<b. I J'

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Page 23: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

4 f I S A S i P

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Page 24: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

11.

t h e s t e e l 28,,000 k s i ( T e s t s showed t h a t E q a c t u a l l y

a v e r a g e d a b o u t 4,800 k s i and E was 27,800 k s i ) . s

However, no a t t e m p t was made t o a d j u s t t h e assumed

s t r e s s l o s s e s b e c a u s e t h e y a r e m a i n l y g o v e r n e d by t h e

e f f e c t of s h r i n k a g e and t h e r e l a x a t i o n of t h e s t e e l .

The d i f f e r e n c e o f 750 k s i i n t h e v a l u e o f E g i v e s

o n l y an e r r o r o f 3.5$.

b) C r e e p c o e f f i c i e n t was assumed t o be C q = 2.5.

c) A s h r i n k a g e c o e f f i c i e n t o f 0.003 x 60$ .= 0.0018 was

assumed b e c a u s e of the v e r y d r y mix u s e d .

d) R e l a x a t i o n o f t h e s t e e l was assumed a t 4$.

C o r r e c t i o n v a l u e s f o r s t r e s s l o s s e s due t o t h e e l a s t i c

s h o r t e n i n g o f t h e p r e s t r e s s i n g b e d , t o v a r i a t i o n s i n s e t t i n g

t h e hand s c r e w j a c k , and t o t h e u n a v o i d a b l e s l i p p a g e o f the

g r i p s , were o b t a i n e d f r o m p r e v i o u s t e s t s . The maximum v a l u e ,

w h i c h was f o u n d to be 660 l b s . f o r a 1/2 i n . d i a m e t e r s t r a n d ,

was t a k e n i n t o a c c o u n t when t h e r e q u i r e d i n i t i a l s t r e s s i n g

f o r c e s were c a l c u l a t e d .

A l l s t r u t s had a b u i l t - i n s t e e l p l a t e 1/4 i n . t h i c k t o

accommodate t h e a d j u s t a b l e h e a d , as shown i n P i g u r e 2. T h i s

p l a t e was a n c h o r e d i n t o t h e c o n c r e t e by two 1/4 i n . d e f o r m e d

b a r s , The ends of t h e s t r u t s were r e i n f o r c e d w i t h l i g h t mesh

i n o r d e r t o d i s t r i b u t e c r a c k s when t e n s i o n , due t o t h e

e c c e n t r i c l o a d a p p l i c a t i o n , o c c u r r e d . The s t r a n d s were c u t

f l u s h w i t h t h e p l a t e and g r o u n d o f f by a c a r b o r u n d u m g r i n d e r

a f t e r d e t e n s i o n i n g was c o m p l e t e d .

T h r e e s i d e s of, t h e s t r u t s had c o a t e d p l y w o o d f o r m f i n i s h .

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F i g . 2 - D e t a i l s o f t h e End P l a t e and t h e F a s t e n i n g Device.'

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13. One 8 i n . s i d e was s t e e l t r o w e l l e d . A l o n g t h e m i d d l e two

f e e t e x c e p t i o n a l c a r e was t a k e n t o t r o w e l the s u r f a c e t o t h e

r e q u i r e d l e v e l and t o keep t h e t h i c k n e s s of t h e s p e c i m e n

w i t h i n an a c c u r a c y o f 1/32 i n . ( M e a s u r e m e n t s o f t h e a c t u a l

u n i t s p r o v e d t h a t t h e d i m e n s i o n s were k e p t c l o s e l y w i t h i n t h e

s p e c i f i e d t o l e r a n c e s ; h o w e v e r , t h e c u r v a t u r e of t h e s t r u t s i n

t h e w eaker d i r e c t i o n v a r i e d b e t ween z e r o and 1/4 i n . ) .

The s p e c i m e n s were i n d i v i d u a l l y numbered and the c o r r e s ­

p o n d i n g c y l i n d e r s had marks r e f e r r i n g t o a l l s p e c i m e n s c a s t

f r o m t h e same b a t c h . Of t h e 37 s t r u t s m a n u f a c t u r e d two had t o

be r e c a s t s i n c e i t was s u s p e c t e d t h a t s t r a n d s l i p p a g e had

o c c u r r e d . Seven o f them were d i s c a r d e d b e c a u s e of d i s c r e p ­

a n c i e s i n d i m e n s i o n s o r e x c e s s i v e c u r v a t u r e .

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I V . PREPARATION OF THE SPECIMENS

M i x i n g o f C o n c r e t e

The b a t c h was m i x e d i n a 1 / 3 c u . y d . t u r b i n e m i x e r .

A l l i n g r e d i e n t s were w e i g h b a t c h e d . E l k , Type I I I h i g h

e a r l y s t r e n g t h bagged cement was u s e d . P r i o r t o manu­

f a c t u r i n g , t h e e n t i r e q u a n t i t y of t h e cement was p u r c h a s e d

and s t o r e d f o r t h e j o b .

The m i x i n g t i m e and s e q u e n c e of t h e b a t c h i n g were

a l s o k e p t c o n s t a n t t h r o u g h o u t t h e work. The t i m e o f m i x i n

was s e t a t t h r e e m i n u t e s measured f r o m t h e t i m e of a d d i n g

w a t e r t o t h e cement. O n l y one b a t c h was u s e d f o r a d a i l y

p r o d u c t i o n and n o r m a l l y t h r e e s t r u t s were c a s t f r o m t h i s

b a t c h . ( E x c e p t i o n s were made when r e c a s t i n g was n e c e s s a r y

o r when, i n one i n s t a n c e , a s p e c i a l t y p e of s t r a n d was n o t

a v a i l a b l e . y I n t h e s e c a s e s o n l y one or two s t r u t s were

c a s t ) .

Bed E q u i p m e n t and S t r e s s i n g

T h r e e i d e n t i c a l l y made s t e e l s t r e s s i n g beds were u s e d

f o r f a b r i c a t i n g the s p e c i m e n s ( F i g u r e 3 ) . The s t r e s s i n g

was p e r f o r m e d by c o n v e n t i o n a l s t r e s s i n g j a c k s r e s t i n g

a g a i n s t a l o a d c e l l . To a v o i d s t r e s s l o s s e s due t o a n c h o r

s l i p p a g e a s p e c i a l l y d e s i g n e d s c r e w - a n c h o r was s c r e w e d

a g a i n s t a s p l i c i n g g r i p a f t e r s t r e s s i n g had been c o m p l e t e d

I n t h i s way t h e a n c h o r s l i p p a g e was e l i m i n a t e d b e c a u s e t h e

wedges i n t h e s p l i c i n g g r i p s y s t e m were a l r e a d y s e t when

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i

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F i g . 3 - D e t a i l s o f t h e S t r e s s i n g E q u i p m e n t .

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16.

the a d j u s t a b l e support of the screwjack was t i g h t e n e d .

F i gu re 4 shows the procedure s c h e m a t i c a l l y .

During the s t r e s s i n g procedure an i n i t i a l p r e - l o a d i n g

was a p p l i e d to e l i m i n a t e g r i p s l i ppage at the f a r end, and

then the j a c k i n g was cont inued to the r equ i red v a l u e . The

converted load c e l l readings are t abu l a ted i n Table II t o ­

gether with a l l data of the manufactur ing procedure.

Res in coated plywood was used f o r the forms to avo id

b l e e d i n g through the j o i n t s . The s ide forms were b o l t e d

to the s t r e s s i n g bed by a dev ice which ensured the proper

p o s i t i o n of the s ide forms at r e - s e t t i n g . The su r f aces of

the plywood not i n contact with the concrete were a l so

t r e a t e d with s h e l l a c to minimize warping of the forms dur ing

s teaming.

P l a c i n g the Concrete

The s t r e s s i n g bed was p laced by an overhead crane onto

a v i b r a t i o n t a b l e . Two e x c e n t r i c s performed the v i b r a t i o n .

The ampl itude and r e v o l u t i o n of the e x c e n t r i c s were set to

s u i t the load of the po r tab le s t r e s s i n g beds and the u n i t s .

V i b r a t i o n time was kept constant and was d i r e c t e d by a

q u a l i t y c o n t r o l l e r . A f t e r v i b r a t i o n the s t r e s s i n g bed was

removed from the v i b r a t i o n tab le and p laced i n to a steaming

k i l n . Before the hood of the k i l n was p laced the f i n i s h i n g

of the sur face was completed.

A s p e c i a l h o l d i n g dev ice was mounted to the v i b r a t i o n

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17.

W O O D E N S O F F I T <t>T £ E I N £f JA6IC

(7) 6,IZIP

F I X E D E N D WOODEN SOFE I J

F i g . 4 - Schematic D e s c r i p t i o n of the S t r e s s i n g Procedure.

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18.

t a b l e and a l o n g w i t h one of t h e u n i t s t h e s i x c y l i n d e r s

were v i b r a t e d i n t h e same mode as t h e s p e c i m e n s . T h i s

way a b e t t e r a p p r o a c h t o f i n d i n g t h e t r u e Young's Modulus

of t h e s p e c i m e n was a n t i c i p a t e d .

4) C u r i n g and D e s t r e s s i n g of t h e S p e c i m e n s

The s t r u t s were c a s t i n t h e m o r n i n g b e f o r e c o n c r e t i n g

of p l a n t p r o d u c t i o n b e g a n . A f t e r 9 t o 11 h o u r s p r e s e t t i m e

t h e u n i t s were c u r e d a l o n g w i t h t h e p l a n t p r o d u c t i o n u n d e r

l o w - p r e s s u r e s t e a m , l a s t i n g . a p p r o x i m a t e l y 9 t o 12 h o u r s , a t

an a v e r a g e t e m p e r a t u r e o f 140°F.

Some of t h e u n i t s were n o t s t e a m e d , b u t were l e f t f o r

a few days u n d e r a p o l y e t h y l e n e c o v e r a t room t e m p e r a t u r e .

A f t e r two of t h e s i x c y l i n d e r s were t e s t e d t o d e t e r m i n e

t h a t t h e minimum 3,000 p s i t r a n s f e r s t r e n g t h had been r e a c h e d ,

t h e s p e c i m e n s were d e s t r e s s e d . F i r s t t h e n u t s of t h e s c r e w -

j a c k s were r e l e a s e d , t h e n t h e s l a c k e n e d s t r a n d s were c u t by

a g r i n d e r .

When the s p e c i m e n s were removed f r o m t h e f o r m s , t h e y

were f i r s t t i l t e d upwards and t h e n l i f t e d . A f t e r s t r i p p i n g ,

t h e u n i t s were s t o r e d t o g e t h e r w i t h t h e c y l i n d e r s u n d e r a

r o o f . No f u r t h e r c u r i n g was p e r f o r m e d a f t e r t h e u n i t s were

s t o r e d .

5) S h i p m e n t o f t h e S p e c i m e n s

T h r e e days a f t e r t h e l a s t u n i t s were c a s t , a l l s p e c i m e n s

s e l e c t e d f o r t e s t i n g were s h i p p e d t o t h e l a b o r a t o r y and

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19.

s t o r e d t h e r e u n t i l t e s t e d . The s t r u t s a l w a y s r e s t e d ' a t

t h e i r o n e - f i f t h p o i n t s w i t h t h e w i d e r s i d e v e r t i c a l . A t

t h e l a b o r a t o r y t h e u n i t s had t o be t u r n e d o v e r s e v e r a l

t i m e s d u r i n g t h e i r p r e p a r a t i o n f o r t h e t e s t i n g . T h i s was

a c h i e v e d by r o l l i n g .them c a r e f u l l y o v e r a t t h e i r o n e - f i f t h

p o i n t s . By h a n d l i n g them t h i s way none of t h e s t r u t s , r e ­

g a r d l e s s of t y p e , c o u l d d e v e l o p any c r a c k s . A l l c y l i n d e r s

were i d e n t i c a l l y s t o r e d w i t h t h e s p e c i m e n s .

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V. TEST PROCEDURE

T e s t i n g M a c h i n e

The s p e c i m e n s were t e s t e d i n a T i n i u s O l s o n , 200,000

l b . e l e c t r o - m e c h a n i c a l u n i v e r s a l t e s t i n g m achine h a v i n g a

minimum r e a d i n g i n c r e m e n t o f 200 l b . T h i s m achine p r o v i d e

a c o n s t a n t r a t e o f s h o r t e n i n g b e t w e e n i t s l o a d i n g h e a d s ,

and m e a s u res t h e l o a d d e v e l o p e d i n t h e s p e c i m e n due t o

t h i s s h o r t e n i n g . The l o a d a p p l i c a t i o n on t h e s p e c i m e n was

u n i n t e r r u p t e d f r o m s t a r t t o f a i l u r e and t o o k a p p r o x i m a t e l y

20 m i n u t e s . L a t e r a l d e f l e c t i o n r e a d i n g s were t a k e n a t

l o a d i n c r e m e n t s o f :

2.5 k i p s f o r c e n t r a l l y l o a d e d s t r u t s

1 .5 k i p s f o r e c c e n t r i c i t y o f e / t = 0.1

1.0 k i p f o r e c c e n t r i c i t y o f e / t = 0.5

As soon as t h e d i a l n e e d l e s t o p p e d , i n d i c a t i n g t h a t

t h e s p e c i m e n c o u l d n ot c a r r y more l o a d , t h e machine was

s t o p p e d . A t t h i s u l t i m a t e l o a d ( d e s i g n a t e d P ), a l t h o u g h u

no f u r t h e r p r e s s u r e was a p p l i e d , t h e l a t e r a l d e f l e c t i o n

s t i l l i n c r e a s e d and t h e mode of f a i l u r e was r e c o r d e d .

On some s p e c i m e n s , a f t e r t h e u l t i m a t e l o a d had been

r e c o r d e d , t h e l o a d i n g was c o n t i n u e d i n o r d e r t o i n v e s t i ­

g a t e t h e b e h a v i o u r o f t h e s t r u t s a f t e r b u c k l i n g had

o c c u r r e d . D e f l e c t i o n Measurement

The l a t e r a l d e f l e c t i o n was r e a d by two t r a n s i t i n ­

s t r u m e n t s , p l a c e d 20' f r o m e a c h s h o r t f a c e of t h e s t r u t .

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21 .

A s c a l e w i t h g r a d u a t i o n s of 0.1 i n . was mounted at- t h e

c e n t r e of t h e s t r u t . R e a d i n g s t o 0.01 i n . were e s t i m a t e d .

I n f i v e i n s t a n c e s the l a t e r a l d e f l e c t i o n of t h e head of t h e

m a c h i n e was measured u s i n g a n o t h e r two t r a n s i t s . A l l f i v e

c a s e s p r o v e d t h a t t h e b o t t o m head d i d n o t move a t a l l ; and

t h e t o p head moved a maximum of 0.03 i n . and t h i s movement

t o o k p l a c e a t t h e b e g i n n i n g of t h e l o a d i n g . As s o o n as

t h e l o a d i n g r e a c h e d 5 t o 10 k i p s no f u r t h e r movement of

t h e t o p head c o u l d be o b s e r v e d . I t was assumed t h a t i n

a l l c a s e s t h e l a t e r a l d e f l e c t i o n o f t h e head of t h e machine

was no g r e a t e r t h a n t h e f i v e c a s e s o b s e r v e d .

M e c h a n i s m of t h e S t r u t S u p p o r t s

An a t t e m p t was made t o p r o v i d e a s u p p o r t w h i c h

( a ) s i m u l a t e d an i d e a l h i n g e d s u p p o r t and (b) l o c a t e d t h e

l o a d as a c c u r a t e l y as p o s s i b l e . I n o r d e r t o do t h i s an

a d j u s t a b l e 3/4 i n . t h i c k s t e e l p l a t e was a t t a c h e d t o t h e

1/4 i n . t h i c k s t e e l p l a t e embedded i n t h e end of t h e s t r u t

as shown i n F i g u r e 2. T h i s p l a t e was p r o v i d e d w i t h two

g r o o v e s each h a v i n g a s e m i - c i r c u l a r c r o s s s e c t i o n m a c h i n e d

t o an a c c u r a c y of 0.001 i n . S i m i l a r p l a t e s were mounted

a t t h e t o p and b o t t o m heads of t h e t e s t i n g m a c h i n e , and

l u b r i c a t e d r o l l e r s 1/2 i n . i n d i a m e t e r were u s e d i n t h e

m a t i n g g r o o v e s .

I t was assumed t h a t t h i s a r r a n g e m e n t k e p t t h e f r i c t i o n

c o e f f i c i e n t a t an a v e r a g e of 0.025. Thus t h e e c c e n t r i c i t y

due t o f r i c t i o n o f t h e h i n g e a t maximum l o a d was l e s s t h a n

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22.

0.01 i n . , and c o u l d be n e g l e c t e d .

Lead shims were l a i d b e t w een t h e two p l a t e s t o t a k e up

p o s s i b l e d i s c r e p a n c i e s i n the embedded s t e e l p l a t e s .

I n o r d e r t o l o c a t e the l o a d as a c c u r a t e l y as p o s s i b l e

t h e a d j u s t a b l e p l a t e was m a n u f a c t u r e d as f o l l o w s :

One g r o o v e was l o c a t e d a t t h e c e n t r e of t h e a d j u s t a b l e

p l a t e and t h e o t h e r e x a c t l y 1.5 i n . away. T h e r e f o r e by

l o c a t i n g t h e c e n t r e g r o o v e a t t h e r e q u i r e d p o s i t i o n ( a l o n g

t h e e s t a b l i s h e d a x i s of t h e s t r u t ) t h e 1.5 i n . e c c e n t r i c i t y

was a u t o m a t i c a l l y o b t a i n e d . F o r t h e 0.3 i n . e c c e n t r i c i t y

the e n t i r e a d j u s t a b l e p l a t e was s e t by t h e thumb s c r e w s so

t h a t t h e m i d d l e g r o o v e was o f f s e t 0.3 i n . f r o m t h e a x i s of

the s t r u t ( F i g u r e 2 ) .

I n o r d e r t o e s t a b l i s h t h i s a x i s a t r a n s i t was s e t up

o v e r t h e c e n t r e p o i n t of t h e s h o r t f a c e . A f t e r e n s u r i n g

t h a t t h e s t r u t was r e s t i n g plumb a s t r a i g h t l i n e was e s t a b ­

l i s h e d , by means of t h e t r a n s i t , t h r o u g h t h i s p o i n t p a r a l l e l

t o a l i n e j o i n i n g t h e m i d - p o i n t s of t h e two ends o f t h e

member. The measured e c c e n t r i c i t y of l o a d i n g was w i t h

r e s p e c t t o t h e c e n t r e s e c t i o n .

The d i s t a n c e b e t w e e n t h e c e n t r e s of t h e end s e c t i o n s

and t h e s t r a i g h t l i n e wa.s t h e measure of the c u r v a t u r e of

t h e s t r u t s , and was r e c o r d e d i n T a b l e I I I i n Column 11.

When l a r g e (1.5 i n . ) e c c e n t r i c i t y was u s e d t h e a d j u s t ­

a b l e p l a t e s were a l s o t i e d t o t h e s i d e o f t h e column ( s e e

P h o t o 1) . The f o r c e , r e q u i r e d t o d e v e l o p a d e q u a t e f r i c t i o n

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23.

PHOTO 1 The F a s t e n i n g D e v i c e f o r t h e A d j u s t a b l e P l a t e .

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24.

b e t w e e n the c l a m p s and the s i d e of the s t r u t , was c r e a t e d

by t i g h t e n i n g t h e b o l t s c o n n e c t i n g t h e two a n g l e i r o n s

t o g e t h e r ( F i g u r e 2 ) . T h i s a r r a n g e m e n t was b e l i e v e d t o be

n e c e s s a r y b e c a u s e i t was f e a r e d t h a t the embedded p l a t e

w o u l d n o t t r a n s m i t t h e moment i n t o t h e s t r u t . A f t e r t h e

a l i g n m e n t was e s t a b l i s h e d as a c c u r a t e l y as p o s s i b l e , t h e

l o c k i n g s c r e w s were t i g h t e n e d and t h e s t r u t was l i f t e d i n t o

i t s f i n a l p o s i t i o n ( s e e P h o t o 2 ) .

W i t h t h i s a r r a n g e m e n t no f u r t h e r a d j u s t m e n t , c h e c k i n g ,

o r o t h e r work was n e c e s s a r y w h i l e t h e s p e c i m e n s were p l a c e d .

A f t e r the s t r u t s were p l a c e d i n t o t h e m achine an i n i t i a l

300 l b . l o a d was k e p t on them u n t i l t h e l i f t i n g c l a m p s

were removed and d e f l e c t i o n t a r g e t s mounted. U s i n g the l o a d

i n c r e m e n t s p r e v i o u s l y m e n t i o n e d , t h e t e s t l a s t e d a p p r o x i ­

m a t e l y 20 t o 25 m i n u t e s . An a v e r a g e o f t h r e e t e s t s was

p e r f o r m e d e a c h day. The c r i t i c a l v a l u e s of two s p e c i m e n s

(No. 10 and No. 13) seemed t o be o u t of l i n e , and i n o r d e r

t o e n s u r e r e l i a b l e a v e r a g e s , t e s t s of a d d i t i o n a l s p e c i m e n s

were d e s i r e d . S i n c e no s p a r e s t r u t s were c a s t t h e s e add-'

i t i o n a l s p e c i m e n s were t a k e n f r o m t h o s e a l r e a d y t e s t e d w i t h

l a r g e e c c e n t r i c i t y (No. 36 and No. 3 7 ) . I n t h e s e c a s e s

c a r e was t a k e n t o e n s u r e t h a t t h e e x p e c t e d t e n s i o n w o u l d

o c c u r on t h e s i d e p r e v i o u s l y u n d e r c o m p r e s s i o n .

S p e c i a l T e s t s

Two c o n t r o l t e s t s were a l s o c a r r i e d out as f o l l o w s :

a) A t e s t t o e s t a b l i s h t h e i n f l u e n c e of p o s s i b l e s m a l l

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PHOTO 2. The Strut During Testing.

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26.

e c c e n t r i c i t y i n t h e d i r e c t i o n p e r p e n d i c u l a r t o

b u c k l i n g . S t r u t No. 36 was so t e s t e d , once w i t h

1 / 8 i n . and once w i t h 1 1 / 8 i n . e c c e n t r i c i t i e s .

These were o b t a i n e d by t i l t i n g t h e s p e c i m e n r e l a t i v e

t o t h e b e a r i n g p l a t e (by means of t h e h o l d i n g s c r e w s )

u n t i l the r e q u i r e d e c c e n t r i c i t y was o b t a i n e d a t the

t o p . The t e s t f o r b o t h e c c e n t r i c i t i e s was c a r r i e d t o

u l t i m a t e l o a d , t h i s b e i n g p o s s i b l e b e c a u s e t he s t r u t

r e m a i n e d u n c r a c k e d ( b e i n g h i g h l y p r e s t r e s s e d ) . The

u l t i m a t e l o a d s f o r t h e s e two c o n d i t i o n s were 54.2 k i p s

and 57.2 k i p s . S i n c e t h e s e a r e w i t h i n a b o u t s i x p e r

c e n t , of e a c h o t h e r , no c o r r e c t i o n f o r p o s s i b l e

e c c e n t r i c i t y i n t h i s d i r e c t i o n was made.

F l e x u r a l modulus of f i v e s p e c i m e n s was a l s o e s t a b ­

l i s h e d by c a r r y i n g out b e n d i n g t e s t s f o r c o m p a r i s o n

w i t h t h e v a l u e s o b t a i n e d f r o m the c y l i n d e r t e s t s .

S t r u t s Nos. 34, 36, 3 7 , 3 8 and 39 were so t e s t e d . The

s p e c i m e n s were s u p p o r t e d on t h e i r w i d e r s i d e 15 i n .

f r o m t h e i r ends and l o a d e d w i t h one c o n c e n t r a t e d l o a d

a t t h e m i d s p a n . Two i n d i c a t o r d i a l s were p l a c e d on

b o t h s i d e s o f t h e s t r u t s a t t h e l o c a t i o n o f t h e l o a d ,

and t h e a v e r a g e of t h e two r e a d i n g s was t a k e n as a

measure o f the d e f l e c t i o n . I n o r d e r t o a v o i d c r a c k i n g

of t h e s p e c i m e n s t he l o a d i n g was c a r r i e d o n l y t o a

v a l u e w h i c h p r o d u c e d a maximum t e n s i o n s t r e s s o f

200 p s i . The c o n c e n t r a t e d l o a d was a p p l i e d i n 250 l b .

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27.

i n c r e m e n t and l o a d d e f l e c t i o n c u r v e s were drawn. The

p l o t s f e l l a l o n g a s t r a i g h t l i n e i n d i c a t i n g t h a t t h e

s e c t i o n s d i d n o t c r a c k d u r i n g t e s t i n g . From the

o b s e r v e d l o a d and c o r r e s p o n d i n g d e f l e c t i o n r e a d i n g s

t h e modulus was c a l c u l a t e d . O n l y f i v e t e s t s were so

c a r r i e d o u t .

C y l i n d e r T e s t s

A B a l d w i n H y d r a u l i c T e s t i n g M a c h i n e t e s t e d t h e c y l i n d e r s

a t t h e t i m e of l o a d i n g . F o r each c y l i n d e r a s t r e s s - s t r a i n

c u r v e was e s t a b l i s h e d , b u t the c o m p r e s s o m e t e r ( s t r a i n -

gauge) was always- removed when t h e c o n c r e t e s t r e n g t h a p p r o a c h ­

ed i t s e x p e c t e d u l t i m a t e v a l u e , so t h a t t h e u l t i m a t e s t r a i n

was n o t o b t a i n e d .

Page 41: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

V I . TEST RESULTS

Gene r a l

• Tb/e" r e s u l t s o f the^'te'Sts .are' g i v e n 1 an' T a b l e , Li?r, and

g r a p h s o f t h e c r i t i c a l l o a d s o b t a i n e d by t h e S o u t h w e l l 15 16

method, ' d i s c u s s e d i n C h a p t e r V I - 3 , a r e p l o t t e d

i n F i g u r e s . 5 , 6 and 7. I t i s n o t i c e a b l e t h a t i n s p i t e

o f t h e c a r e t o s i m u l a t e i d e a l l a b o r a t o r y c o n d i t i o n s

t h e v a l u e s have c o n s i d e r a b l e s p r e a d . F o r z e r o e c c e n ­

t r i c i t y t h e y v a r y b e t w e e n 5 8 . 2 k i p s and 7 8 . 0 k i p s , and

f o r 0 . 3 i n . l o a d e c c e n t r i c i t y b e t ween 4 6 . 0 k i p s and

6 2 . 3 k i p s . I n o r d e r t o e l i m i n a t e the e f f e c t o f d i f f e r e n t

m o d u l i on t h e c r i t i c a l l o a d a l l v a l u e s o b t a i n e d f r o m t h e

S o u t h w e l l P l o t s were c o n v e r t e d t o v a l u e s c o r r e s p o n d i n g

t o an i d e n t i c a l m o d u l u s , a r b i t r a r i l y c h o s e n . T h i s

a r b i t r a r i l y c h o s e n v a l u e was s e t a t E' = 3 .320 k s i , a

v a l u e 5$ l e s s t h a n t h e one o b t a i n e d f r o m t h e ' l o w e s t

c y l i n d e r t e s t r e s u l t , i n o r d e r t o a r r i v e a t a c o n v e r s i o n

f a c t o r a l w a y s l e s s t h a n one. The c o n v e r s i o n was made

l i n e a r by m u l t i p l y i n g t h e c r i t i c a l l o a d s , o b t a i n e d f r o m

t h e S o u t h w e l l P l o t s , by t h e r a t i o o f E' = 3 ,320 k s i t o

th e m o d u l i o b t a i n e d f r o m the c o r r e s p o n d i n g s t r e s s - s t r a i n

c u r v e s o f t h e c y l i n d e r t e s t s ( s e e C h a p t e r V I - 4 ) . T h i s

r a t i o i s d e n o t e d i n T a b l e I I I as oc' . The c o n v e r t e d

c r i t i c a l l o a d v a l u e s a l s o show a s p r e a d b e t w e e n 43.7 k i p s

and 58.7 k i p s f o r t h e c e n t r a l l y l o a d e d s t r u t s , and be­

tween 38 .2 k i p s and 56.7 k i p s f o r t h o s e w i t h 0 . 3 i n .

Page 42: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

o < O _)

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d o

70

A C T U A L CRITICAL LOADS V*. p % F<9K A L L 6PECI/WEM^ TESTED WITH O i O.*? ECCENTRICITIES CONVERTED CRITICAL LOADS » 11 11

AVEieA^E.'.4>.9

A 2 0.4 1.0 F i g . 5 C r i t i c a l Loads f o r Specimens w i t h Z e r o and 0.3 i n , .-2 |.T

E c c e n t r i c i t i e s . P 7 ° IV)

Page 43: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

< 0 _ l

< 0

A C T U A L CRITICAL L O A D S V*. p & FOfc < ? P E C I A A E N 6 T E S T E D C O N C E N T R I C A L L Y C O N V E ^ T E P CRITICAL LOAE?4> n « » n . n

AV E K,A4 £ i 6 5 , £8

AVEfcAqe.: 48.2.

o.2 OA o.b o.e> \.o \.t py* F i g . 6 C r i t i c a l Loads f o r Specimens w i t h Z e r o E c c e n t r i c i t y O n l y .

Page 44: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

< A C T U A L CRITICAL L O A D S fO$L S p E C I A A E N T E S T E " O W I T H O.h E C C E N T R I C I T Y

-J C O N V E R T E D CRITICAL L<9AD€» » " •• n

P i g . 7 C r i t i c a l Loads f o r S p e c i m e n s w i t h 0 . 3 i n . E c c e n t r i c i t y O n l y .

Page 45: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

32. e c c e n t r i c i t y .

Table I I I shows the t e s t specimens d i v i d e d i n t o f i v e

main groups a c c o r d i n g to t h e i r s t e e l r a t i o s , and w i t h i n

these groups s e p a r a t e d a c c o r d i n g to the l o a d e c c e n t r i c i t i e s

used under the heading Test Data. There i s a l s o r e f e r e n c e

to the amount of s t e e l and the c o r r e s p o n d i n g i n i t i a l s t r e s s ,

and Column 6 shows the time i n days which e l a p s e d between

c a s t i n g and t e s t i n g .

T a b u l a t e d O b s e r v a t i o n s

Two c h a r a c t e r i s t i c l o a d r e a d i n g s are shown i n Table I I I .

Under Column 8 l o a d s c o r r e s p o n d i n g to the l a s t r e a d i n g at

which l a t e r a l d e f l e c t i o n c o u l d be observed are shown as

P ' . The l a t e r a l d e f l e c t i o n c o r r e s p o n d i n g to P ' i s r e c o r d e d

as S under Column 9. The u l t i m a t e l o a d , as r e c o r d e d by the

machine d i a l , d e s i g n a t e d P ^ , i s i n Column 7. I n v a r i a b l y t h i s

l o a d i s l e s s than a f u l l increment g r e a t e r than P ' .

In a l l cases of specimens w i t h zero and 0.3 i n .

e c c e n t r i c i t i e s , when the l o a d approached i t s u l t i m a t e P

v a l u e , the r a t e of the l a t e r a l movement of the c e n t r e of the

s t r u t suddenly i n c r e a s e d , and at t h i s p o i n t no f u r t h e r

d e f l e c t i o n r e a d i n g s were p o s s i b l e . Meanwhile the d i a l

i n d i c a t o r reached the maximum r e a d i n g and then the l o a d

dropped to a v a l u e at which the l a t e r a l movement a l s o

stopped. The s t r u t s kept r e s i s t i n g t h i s reduced l o a d and

the c o r r e s p o n d i n g d e f l e c t i o n s v a r i e d *;between 0.6 i n . and

3.5 i n . depending on the nat u r e of the b u c k l i n g .

Most of the s t r u t s w i t h s m a l l percentage of s t e e l

Page 46: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

T A. O e. P V A T I c?K<5 C A- t . CU L As T 1 <S> SJ S> 1. 3. 4-. 5. 7. \o. II . VL. 13. I4- 15. 16. 17- \e>. 1 19. 'LO.

MIC P i i "co T Pu p' S

r l

\- ao <3| Per r c - ) 1

OC oc'fcr — % IN. psi. IN. IN. IN- ICS I. PSI. psi- —

,1 0 0 .23 1-5/16 328 86 66.0 62 . 5 . 11 ^8973 .094 .01 5 72.0 4833 124 3048 3698 . 2398 .69 49.7 1 2 75 54.2 52.5 .58 8770 .063 . 1 27 63.O 4683 1 24 2555 561 5 -T545 .71 44.7

67.5 47.2 1 7 0.1 77 32.9 31 .5 .47 7652 .280 .212 46.0 401 7 1 31 1 684 3479 -.111 .83 38.2 24 97 37.4 36.0 .57 6509- -.117 .290 54.0 3638 1 28 1 681 4271 -'909 .91 49. 1 24 37.4

50 ;o 43.7 25 0.5 96 12.1 12.0 .65 7087' -. 1 25 - - 4093 1 37 789 2609 -1 0,31 -29 96 10.7 10.0 .43 6448 . 1 32 - - 3685 1 37 748 2348 - 852 - -31 100 11.6 11.0 .48 - .000 - - - 1 37 789 2609 -1 031 - -

1 8 0 .45 1-7/6 635 76 58.9 57.5 .20 8328 .063 .036 69.0 4595 1 25 3020 41 70 1 870 .73 50.4 1-7/6 76 48.4 47.5 .29 7290 .01 6 .067 58.2 4407 1 26 2540 3980 1 280 .75 43.7 76 48.4 47.5 .29

63.6 47. 1 1 5 0.1 77 32.9 32.5 .62 7652 .074 .31 2 50.0 401 7 1 31 1 964 4484 ' - 556 .83 41 .5 35 68 41 .0 40.5 .65 7397 . 1 02 . 200 54.0 41 1 3 1 29 2293 5153 - .567 .81 43. 7 35 41 .0 40.5 .65 7397

52.0 -1 461

42 . 6 28 0.5 96 12.5 12.5 .70 6448 . 1 40 - - 3685 1 36 839 31 39 -1 461 - -30 1C0 12.5 12.0 .53 - . 1 25 - - - 1 37 830 2860 -1 200 — -1 1 0 .60 1 -1/2 . 840 86 65.0 62 . 5 .22 8973 .055 .020 67.5 4833 1 24 3460 4730 21 90 .69 46.6 1 4 75 ' 57.5 55.0 .70 8770 .063 .060 62.5 4683 1 26 31 50 6610 - 3 1 0 .71 44.4 1 4 75 ' 57.5 55.0 .70 8770 .063

65.0 45.5 23 0.1 97 37.4 36.0 .55 6509 .047 .260 52.9 3638 1 28 2330 4750 - 90 .92 48.7 26 96 49'. 0 •49.0 .51 7087 . 1 88 .092 50.0 4093 1 27 2807 5257 - 357 .82 41 .0 26 96 49'. 0 •49.0 .51 7087 .092

51 .5 44.8 38 0.5 64 13.9 13.0 .65 7228 .110 - - 3972 136 • 871 3210 -1 469 - -39 65 14.3 14.0 ..75 7228 . 1 25 - - 3972 136 91 3 3533 -1 707 — —

TABLE I I I ' . - TEST RESULTS ' ( C o n t i n u e d ) ^

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D A. • T A U U A T I O N S 1.. '2. 3 . 4-- 5 . (o. 7. 8. IC II • 13. I4-- 15. \<o. 17- 10. \o>- io .

MK r ( ) 'co T Pu p' 5 o Qo Per Et "su (To <*fcr

— % I KJ - P6I. DAY I4IPS KIPS IN- psi. IN. iN- KIPS KSI. Psi. PSI- psi . — KIPS 9 0 .91 2-7/6 1 275 86 62 „ 5 6 0 . 0 .34 8973 . 0 0 0 .040 6 7 . 3 4833 1 25 3320 L 5200 1 440 .69 4 6 . 4

1 3 1D9 72,5 7 0 . 0 . 1 0 8973 .055 .01 2 7 8 . 0 4683 1 22 41 35 4790 3480 .71 55 .4 34 64 57 . 2 5 5 . 0 . 3 8 721 3 .079 ,030 6 0 . 0 4523 1 25 3450 5330 1 570 .74 4 4 . 4 36 61 54 . 2 52.5 .32 7388 . 1 25 . 1 02 6 8 . 2 3861 1 24 3495 5455 .2045 .86 5 8 . 7

68 .4 5 1 . 2 1 6 0 . 1 77 4 0 . 1 39.0 .70 7652 .440 .310 5 8 . 2 401 7 1 28 2840- 6090 - 410 .83 48.. 3 33 53 34 .3 3 4 . 0 .44 6627 -.226 .225 47 .5 3730 129 2600 4720 - 480 .89 4 2 . 3

52 .9 4 5 . 3 36 0 .5 62 15 .2 1 5 . 0 .89 7388 .01 7 - - 3861 1 36 2990 3945 -2035 - -1 9 20 37

0 1 . 2 0 2 - 1/2" 1680 104 65 61

60 ,0 57 .9 43.6

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6 2 . 8 6 0 . 9 5 9 . 0

4595 4407 3861

1 24 123 1 28

4070 3880 3365

5205 581 0 5995

2935 1 950

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45 . 8 4 5 . 7 50 ,7

1 9 20 37

104 65 61

60 ,0 57 .9 43.6

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4595 4407 3861

47 .4 32 27

0 . 1 53 96

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.47

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4 9 . 3 6 2 . 3

3730 3685

1 28 1 26

31 1 5 3430

5875 7220

- 355 - 360

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27 53 96

3 7 . 8 46 .0

36 . 0 4 5 . 0

.47

.70 . 1 62 .278

5 5 . 8

3730 3685

5 0 . 3 22 37

0 . 5 97 6S

18,0 17.3

18 .0 17 .0

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6509 7388

.090

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134 1 36

1 075 998

4655 41 1 e

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TABLE I I I ' , - TEST RESULTS

Page 48: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

3 5 .

c r a c k e d a f t e r t h e l o a d a p p r o a c h e d i t s u l t i m a t e v a l u e . As

a c o n s e q u e n c e of t h e c r a c k i n g t h e s e s t r u t s s u d d e n l y de­

f l e c t e d 2 i n . t o 3.5 i n . ( s e e an example i n P h o t o 3 ) .

Whereas s t r u t s w i t h l a r g e p e r c e n t a g e of s t e e l d i d n o t c r a c k

and s t o p p e d m o v i n g l a t e r a l l y a t 0.6 i n . t o 1.2 i n . These

were a l l s t r u t s p r e s t r e s s e d w i t h a t l e a s t 1 - 1/2 i n . d i a .

s t r a n d f o r no e c c e n t r i c i t y , and 2 - 7/16 i n . d i a . s t r a n d s

f o r 0.3 i n . e c c e n t r i c i t y . The l o a d d r o p p e d t o a p p r o x i m a t e ­

l y o n e - t h i r d o f i t s u l t i m a t e v a l u e f o r t h e low p r e s t r e s s e d

s t r u t s w h i c h c r a c k e d , and t o 80 - 90$ of i t s u l t i m a t e v a l u e

f o r t h e h i g h p r e s t r e s s e d ones w h i c h d i d n o t c r a c k . A l l

t h e s e o b s e r v a t i o n s t o o k p l a c e w h i l e t h e machine was n o t i n

m o t i o n .

The s t r u t s w i t h 1.5 i n . e c c e n t r i c i t y b e h a v e d d i f f e r e n t ­

l y t h a n t h e ones i n t h e f i r s t two g r o u p s . L a t e r a l d e f l e c ­

t i o n s were l a r g e r t h a n i n t h e o t h e r s p e c i m e n s a t a l l v a l u e s

of l o a d , and when t h e u l t i m a t e l o a d was r e a c h e d , and t h e

l o a d i n g s t o p p e d ;then no f u r t h e r d e f l e c t i o n t o o k p l a c e . I n

most c a s e s t h e l o a d was n o t c o n t i n u e d i n o r d e r t o s a v e t h e

s p e c i m e n s .

F i g u r e s 8/1 t o 8/4 show t h e l o a d d e f l e c t i o n c u r v e s o f

s p e c i m e n s l o a d e d w i t h 1.5 i n . e c c e n t r i c i t y , and F i g u r e 9

shows t h i s g r a p h f o r s t r u t No. 2-9 ( 3 2 8 p s i p r e s t r e s s )

w h i c h was t e s t e d t o d e s t r u c t i o n and f a i l e d i n t e n s i o n

when 3.0 i n . d e f l e c t i o n was r e a c h e d (Photo' 4 ) . S t r u t

No. 22 was a l s o t e s t e d t o d e s t r u c t i o n ; h owever, t h i s

s t r u t w h i c h was h i g h l y p r e s t r e s s e d (1 ,680 p s i ) f a i l e d i n

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36.

PHOTO 3. B u c k l e d S t r u t w i t h Low P r e s t r e s s .

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•co

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F i g . 8/ L o a d - d e f l e c t i o n C u r v e s of S p e c i m e n s w i t h 1 .5 i n . E c c e n t r i c i t i e s .

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io

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STR: UT"? »<?»

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F i g . 8/2 L o a d - d e f l e c t i o n C u r v e s o f S p e c i m e n s w i t h 1.5 i n . E c c e n t r i c i t i e s .

P 1 • l^.O

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to

CL \0

4

2

F i g ,

.4 .5 -7 .e> P & P L - £CJ\OM e> ( IN.)

8/3 L o a d - d e f l e c t i o n C u r v e s o f Sp e c i m e n s w i t h 1.5 i n . E c c e n t r i c i t i e s .

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_ lo

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-

'•2. .?> .4 .5 .7 P E F L E - C T I ^ N "c5 11 (IN-)

-6 .<T*

Pu *

p1 * \e>.o£-

F i g . 8/4 L o a d - d e f l e c t i o n C u r v e s o f S p e c i m e n s w i t h 1.5 i n . E c c e n t r i c i t i e s .

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" p " ST&vj N£ # 9 (e * l .£ I M . )

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PHOTO 4. T e n s i o n F a i l u r e o f S p e c i m e n No. 2 9 ,

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c o m p r e s s i o n a t 1.7 i n . d e f l e c t i o n ( s e e P h o t o 5 ) . T h i s

i n d i c a t e d t h a t t h e c o m p r e s s i v e f i b r e s t r e s s had r e a c h e d

i t s u l t i m a t e v a l u e due t o the c o m b i n a t i o n of t h e b e n d i n g

moment, e x t e r n a l l o a d and t h e p r e s t r e s s i n g f o r c e .

I t was o b s e r v e d t h a t s t r u t s No. 28 and No. 29 c r a c k e d

d u r i n g t e s t i n g a t t h e t e n s i o n s i d e , 6 i n . f r o m t h e b o t t o m

and t h e t o p , a t t h e l o c a t i o n where the f a s t e n i n g a n g l e

i r o n o f t h e h o l d i n g d e v i c e was s e t . No s u c h v i s i b l e

c r a c k s c o u l d be o b s e r v e d f o r t h e r e s t o f t h e s p e c i m e n s .

Column 10 shows t h e a v e r a g e u l t i m a t e s t r e n g t h o f t h e

c o r r e s p o n d i n g f o u r c y l i n d e r s . I n s p i t e o f t h e h i g h l y

c o n t r o l l e d o p e r a t i o n t h e s e v a l u e s v a r i e d b e t w e e n 6,509

p s i • a n d 8,973 p s i .

I n Column 11 t h e o b s e r v e d i n i t i a l c u r v a t u r e of the

s p e c i m e n s a r e shown, d e n o t e d by t h e s y m b o l a Q . These

v a l u e s a r e t h e a v e r a g e s o f t h e f o u r d i s t a n c e s b e t w e e n t h e

e s t a b l i s h e d a x e s and t h e c e n t r e s of t h e s e c t i o n s measured

a t t h e ends of t h e s t r u t s ( s e e C h a p t e r V - 3 ) .

T a b u l a t e d C a l c u l a t i o n s

A) C r i t i c a l L o a d s . - I n Columns 12 t o 20 of T a b l e

I I I a r e shown c a l c u l a t e d v a l u e s as f o l l o w s . The c r i t i c a l

l o a d s were o b t a i n e d by the S o u t h w e l l Method ' . T h i s

method e l i m i n a t e s t h e e f f e c t of t h e i n i t i a l c u r v a t u r e and

th e d i s c r e p a n c i e s of p l a c i n g t h e l o a d s , p r o v i d e d t h a t :

a) t h e d e f l e c t i o n s a r e s m a l l enough t o j u s t i f y t h e

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44.

PHOTO 5. C o m p r e s s i o n F a i l u r e o f S p e c i m e n No. 22.

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a p p r o x i m a t i o n i n t h e e x p r e s s i o n f o r t h e c u r v a t u r e ,

w h i c h i s u s e d t o d e r i v e t h e d i f f e r e n t i a l e q u a t i o n

of a c u r v e d b a r ( i n c o r p o r a t i n g a s m a l l i n i t i a l

c u r v a t u r e o f t h e b a r ) ;

b) t h e d e f l e c t i o n s a r e s m a l l enough t o p r e v e n t

i m p a i r m e n t of the m a t e r i a l d u r i n g t e s t i n g

( c r a c k i n g , y i e l d i n g ) ;

c ) b o t h the d e f l e c t i o n and l o a d a r e l a r g e enough t o

make t h e d e t e r m i n a t i o n o f the r a t i o of t h e

d e f l e c t i o n t o t h e l o a d p o s s i b l e w i t h s u f f i c i e n t

a c c u r a c y ;

d) t h e d i s t a n c e o f t h e i n i t i a l d e f l e c t i o n of t h e

c e n t r a l l i n e f r o m t h e l i n e o f t h r u s t s h o u l d

v a n i s h a t e i t h e r end of t h e s t r u t , o r a t l e a s t be

as s m a l l as p o s s i b l e .

I f t h e s e c o n d i t i o n s a r e met t h e r e l a t i o n s h i p b e t w e e n t h e

l o a d , i n i t i a l c u r v a t u r e and the d e f l e c t i o n c o r r e s p o n d i n g

t o t h e l o a d c a n he e x p r e s s e d by the e q u a t i o n

O = a o ............ a.) P /P -1

c r

The v a l u e s o f S c a n be p l o t t e d a g a i n s t t h e r a t i o h/?

g i v i n g a s t r a i g h t l i n e w h i c h i n t e r s e c t s t h e c o o r d i n a t e

e>/p = 0 a t t h e d i s t a n c e a f r o m t h e o r i g i n . Then t he o

i n v e r s e s l o p e o f t h i s l i n e g i v e s t h e c r i t i c a l l o a d and

t h e d i s t a n c e r e p r e s e n t s the i n i t i a l c u r v a t u r e .

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46.

.Timoshenko, i n h i s " T h e o r y of E l a s t i c S t a b i l i t y " ,

C h a p t e r 4.1, p. 141, f u r t h e r d e v e l o p s t h e S o u t h w e l l P l o t

method f o r use when s m a l l l o a d e c c e n t r i c i t y i s c o m b i n e d

w i t h i n i t i a l c u r v a t u r e . Then t h e e q u a t i o n a.) may b e '

w r i t t e n as S - - ( a + 4e / l t ) 1 . . . . . . . . . . . b . ) 0 P /P-1 c r

T h e r e f o r e , an a t t e m p t was made t o use t h e S o u t h w e l l

Method f o r f i n d i n g t h e c r i t i c a l l o a d s f o r a l l s p e c i m e n s

h a v i n g z e r o and 0.3 i n . l o a d e c c e n t r i c i t i e s . The c o m b i n e d

e f f e c t o f t h e i n i t i a l l o a d e c c e n t r i c i t y and t h e i n i t i a l

c u r v a t u r e ( i n c o r p o r a t i n g a l l m a n u f a c t u r i n g i m p e r f e c t i o n s ) ,

d e n o t e d by the l e t t e r a^ and t a b u l a t e d i n Column 12, a r e

t h e v a l u e s t a k e n f r o m t h e s e S o u t h w e l l P l o t s drawn f o r e a c h

s p e c i m e n . V a l u e s o f a^ i n Column 12 s h o u l d be e q u a l t o

t h e measured v a l u e s a Q i n Column 11 p l u s 4e/TC .

T h e r e were t h r e e s p e c i m e n s (No. 24, No. 25, and No.

33) w h i c h b u c k l e d o p p o s i t e to t h e i r c u r v a t u r e . Two of them

were l o a d e d w i t h 0.3 i n . e c c e n t r i c i t y and t h e t h i r d w i t h

1.5 i n . e c c e n t r i c i t y . The d i f f e r e n c e s b e t w e e n t h e v a l u e s

a.| and (a + 4,e/fC ) must be a t t r i b u t e d t o t h e e x p e r i m e n t a l

e r r o r i n p l a c i n g t h e l o a d , m e a s u r i n g a , and t o t h e f a c t

t h a t t h e e c c e n t r i c i t y e may be of same or o p p o s i t e s i g n t o

t h e v a l u e o f a ( s e e P i g u r e 1 0 ) . 0 Some c h a r a c t e r i s t i c S o u t h w e l l P l o t s a r e shown i n

P i g u r e 11. F i g u r e s 11 / a , 1 l / b , and 1 l / c show e x a m p l e s of the

S o u t h w e l l P l o t done f o r s t r u t s Nos. 10, 20 and 17 h a v i n g

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47.

P I P P ^ ^ M T U0ADIN4 C<9ND!TI0N^ P0K. eaU/SsL ZCC£tilZ\C\V&>. (LATELY EXA^ESLA-TEp)

P. ,p

fclGHTlU^ M O M E N T

0.3 I M .

C E N T R O I P A L A X I 6

£ I 4 H T I M 4 AAOMEKJT D I A C j & A M

* IN.

.SPECIMEN

L -ESTASLIMMED AX|£

LOADING OPNPITI^K 2

F i g . 10. The two Types of Load E c c e n t r i c i t i e s u s e d .

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48.

S T R U T 10.

o.oob

5(114.) F i g . 11/a. T y p i c a l S o u t h w e l l P l o t s ,

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STieUT 20.

F i g . 11/b. T y p i c a l S o u t h w e l l P l o t s .

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. 0 0 4

o

50.

S T R U T 17

Per * °>'^ s 4(r> ^ .00S = =

a{ * 0.112 (IN.)

, 3 - 4 - .5.

S ( l M )

F i g . 1l/c. T y p i c a l S o u t h w e l l P l o t s .

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51 .

e c c e n t r i c i t i e s .015 i n . , .019 i n . and .212 i n C r e s p e c t ­

i v e l y . The p l o t t e d v a l u e s f o l l o w q u i t e a c c u r a t e l y t h e

s t r a i g h t l i n e i n the v i c i n i t y of t h e h i g h e r P v a l u e s .

F i g u r e 11/d ( s t r u t No. 32) i s a s i m i l a r example where,

t h o u g h t h e p l o t s show a s t r a i g h t l i n e p a t t e r n , t h e l a s t

two p l o t s , one of w h i c h i s t h e P , t e n d t o d e v i a t e f r o m u

t h e s t r a i g h t l i n e . F i g u r e 11/e i s an example where o n l y

t h e u l t i m a t e P v a l u e f a l l s above t h e s t r a i g h t l i n e , - an u i n d i c a t i o n t h a t t h e b u c k l i n g a l r e a d y t o o k p l a c e . I t i s

a l s o n o t e w o r t h y t h a t a t t h e b e g i n n i n g of t h e l o a d i n g t h e

p l o t t e d p o i n t s a r e s c a t t e r e d , b e c a u s e a t t h i s r a n g e t h e

a s s u m p t i o n s on w h i c h t h e S o u t h w e l l method i s b a s e d a r e

n o t s a t i s f i e d . A good example i s t h e p l o t of s t r u t

No. 17 i n F i g u r e 1 1 /c .. F u r t h e r m o r e , a c c o r d i n g t o t h e

e x a c t a n a l y s i s t h e s t r u t may f i r s ' t d e f l e c t i n one d i r e c ­

t i o n and l a t e r on s u d d e n l y b u c k l e i n t h e o p p o s i t e d i r e c ­

t i o n . (See T i moshenko "Theory of E l a s t i c S t a b i l i t y " C h a p t e r

4, Page 191, and C h a p t e r 1, Page 1 4 ) . A good example of t h i s

was t h e t e s t of s t r u t No. 13 w h i c h f i r s t d e f l e c t e d e a s t

u n t i l 45 k i p s l o a d was r e a c h e d , t h e n s u d d e n l y d e f l e c t e d

w e s t and f a i l e d a t 72.5 k i p s l o a d .

A f t e r t h e l o a d was removed a r e s i d u a l d e f l e c t i o n of

0.3 i n . e a s t was m e a s u r e d . W i t h t h i s i n i t i a l c u r v a t u r e t h e

s t r u t was r e l o a d e d and f a i l u r e o c c u r r e d a t 49.0 k i p s

l o a d . The S o u t h w e l l P l o t was drawn f o r b o t h c a s e s and

t h e c r i t i c a l v a l u e s 78 k i p s and 76 k i p s o b t a i n e d r e s p e c t ­

i v e l y . T h i s d o u b l e t e s t i s good e v i d e n c e t h a t t h e

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F i g . 1 1 / d . T y p i c a l S o u t h w e l l P l o t s .

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6_ o - (%

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.012

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54.

S o u t h w e l l P l o t i s u s e f u l t o e s t i m a t e t h e c r i t i c a l l o a d

v a l u e .for s t r u t s w i t h any i n i t i a l c u r v a t u r e p r o v i d e d

t h a t t h i s c u r v a t u r e i s s m a l l .

A n o t h e r r e a s o n f o r t h i s e r r a t i c p l o t was t h a t a t t h e

b e g i n n i n g t h e s t r u t s moved u n t i l t h e y f o u n d t h e i r f i n a l

p o s i t i o n i n t h e m a c h i n e . As a l r e a d y m e n t i o n e d i n

C h a p t e r V-2, t h e t o p head moved a p p r o x i m a t e l y 0.02 t o

0.03 i n . a t t h e b e g i n n i n g o f t h e l o a d i n g w h i c h l e a d s t o

f a l s e d e f l e c t i o n m e a s u r e m e n t s. B u t t o w a r d s t he end o f

t h e l o a d i n g t h e movement d i d n o t o c c u r and t h u s d i d n o t

a f f e c t t h e v a l i d i t y o f t h e r e a d i n g s .

P l o t s o f f i v e s p e c i m e n s f r o m t h e f i r s t two g r o u p s ,

h o w e v e r , d i d n o t show c l e a r s t r a i g h t l i n e p a t t e r n ( s t r u t s

Nos. 13, 19, 26, 27 and 3 3 ) . I n t h e s e c a s e s two o r more

l i n e s c o u l d be drawn w i t h e q u a l j u s t i f i c a t i o n . P i g u r e

1 l / f shows t h e S o u t h w e l l P l o t o f No. 33 as an 'example.

A l t h o u g h i t was d o u b t f u l t h a t t h e c r i t i c a l l o a d s ob­

t a i n e d f r o m t h e S o u t h w e l l P l o t s f o r s p e c i m e n s w i t h 1.5 i n .

l o a d e c c e n t r i c i t y w o u l d y i e l d r e l i a b l e r e s u l t s , an a t t e m p t

was made t o draw t h e S o u t h w e l l P l o t s f o r t h e s e s p e c i m e n s as

w e l l . F i g u r e s 11/g, 11/h and 1 l / i show t h r e e e x a m p l e s .

The a v e r a g e r a t i o o f P t o P c r i s 0.83 f o r t h e g r o u p ,

w i t h " z rero7 and 1 0 . 73' t or' t h e gr'oupr w i t h " 0 . 3 'in' , ' " e c c e n t r i c i t y .

The ' r a t i o s * do n o t " a p p e a r 1 t o ̂ depend '.'on t h e " s t e e l ' ' r a t i o as

s h o w h " " i n - F i g u r e 12.

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S T K U T 33 '

F i g . 1 1 / f . T y p i c a l S o u t h w e l l P l o t s .

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F i g . 11/g. T y p i c a l S o u t h w e l l P l o t s .

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F i g . 1 1 / i . T y p i c a l S o u t h w e l l P l o t s .

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F i g . 12. V a r i a t i o n of R a t i o P /P w i t h S t e e l C o n t e n t . u c r

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Under the main h e a d i n g o f " c a l c u l a t i o n s " i n T a b l e I I I

a r e shown t h e v a l u e s of the t a n g e n t m o d u l i o b t a i n e d a t

t h e a n t i c i p a t e d c o m p r e s s i v e s t r e s s l e v e l , g r a p h i c a l l y

e s t a b l i s h e d f r o m t h e s t r e s s - s t r a i n c u r v e s ( s e e C h a p t e r

' V I - 4 ) . They a r e a v e r a g e s o f t h e c o r r e s p o n d i n g f o u r

c y l i n d e r t e s t r e s u l t s and t h e i r v a l u e s v a r y b e t w e e n

3,832 k s i and 4,833 k s i .

B) S t r e s s e s . - I n T a b l e I I I Columns 16, 17, and 18

show t h e c a l c u l a t e d s t r e s s e s c o r r e s p o n d i n g t o t h e P '

v a l u e s . The P v a l u e s c o u l d n o t be u s e d f o r t h e s e u c a l c u l a t i o n s b e c a u s e t h e c o r r e s p o n d i n g d e f l e c t i o n

measurements were n o t a v a i l a b l e , as a l r e a d y n o t e d . I n

Column 16 t h e a v e r a g e c o m p r e s s i v e s t r e s s e s , d e n o t e d by

(3c due t o t h e p r e s t r e s s i n g f o r c e and P ' a r e t a b u l a t e d .

The p r e s t r e s s i n g f o r c e s d e c r e a s e due t o t h e s u p e r i m p o s e d

P ' l o a d s and t h e i r v a l u e s , d e n o t e d by t h e l e t t e r s f , J su

a r e shown i n Column 15. I n o r d e r t o c a l c u l a t e t h e

e x t r e m e f i b r e s t r e s s e s , d e n o t e d by C 3 { ^ + ' on t h e c o m p r e s s ­

i o n s i d e and (j on the t e n s i o n s i d e , t h e moment due to'

th e l o a d P ' a c t i n g a t t h e l e v e r arm (& + oxt) was s u p e r ­

i m p o s e d on (j & and t h e r e s u l t s t a b u l a t e d i n Columns 17

and 18 r e - s p e c t i v e l y . When s t r e s s l o s s e s were c a l c u l a t e d

t h e c o r r e s p o n d i n g E^ v a l u e s were t a k e n i n t o a c c o u n t and

the v a l u e E g was t a k e n t o be 27,800 k s i f r o m t h e a c t u a l

m i l l c e r t i f i c a t e s . Thus t h e e f f e c t o f the v a r i a t i o n i n n

i s a l s o i n c o r p o r a t e d i n t h e s e v a l u e s . The c a l c u l a t i o n s

assumed an u n c r a c k e d s e c t i o n , u s i n g t h e g r o s s s e c t i o n of

Page 74: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

61 .

t h e s t r u t i n s t e a d of t h e t r a n s f o r m e d s e c t i o n . T h i s

a p p r o x i m a t i o n g i v e s an e r r o r o f l e s s t h a n 1$. The e f f e c t

o f t h e f r i c t i o n o f t h e h i n g e s was a l s o i g n o r e d .

F i b r e s t r e s s e s of s t r u t s w i t h 1.5 i n . e c c e n t r i c i t y -

were a l s o c a l c u l a t e d u s i n g e l a s t i c a n a l y s i s f o r v a l u e s of

P u/2 a t w h i c h t h e s p e c i m e n s s t i l l b e h a v e d e l a s t i c a l l y .

The v a l u e s a r e compared i n T a b l e i v / a w i t h s t r e s s e s

c a l c u l a t e d by a m o d i f i e d S e c a n t f o r m u l a

A c + A c [ > p + 1/ \^TJ r \4E^r) j

3

d e v e l o p e d f o r p r e s t r e s s e d c o n c r e t e s t r u t s by B r e c k e n r i d g e .

I n u s i n g t h e m o d i f i e d s e c a n t f o r m u l a t h e v a l u e s were t a k e n

f r o m T a b l e I I I .

The e l a s t i c a n a l y s i s o f s t r e s s e s c o r r e s p o n d i n g t o t h e

u l t i m a t e l o a d ( T a b l e i v / b ) i n d i c a t e s t h a t a l l s p e c i m e n s i n

t h i s g r o u p c r a c k e d , and the b e h a v i o u r of the s t r u t s must

be a n a l y s e d i n e l a s t i c a l l y .

F i g u r e s 13/a and 13/b show t h e c u r v e s of t h e m o d i f i e d

s e c a n t f o r m u l a p l o t t e d f o r t h e t e s t s p e c i m e n s c o r r e s p o n d i n g

t o t h e s m a l l e s t and l a r g e s t p e r c e n t a g e of s t e e l and 4 , 3 0 0

k s i f o r t h e modulus o f c o n c r e t e .

C a l c u l a t i o n o f t h e M o d u l i

F i n a l l y , T a b l e I I I shows the m o d u l i , d e n o t e d by t h e

l e t t e r o b t a i n e d f r o m the s t r e s s - s t r a i n c u r v e s of the

t e s t c y l i n d e r s a t t h e a n t i c i p a t e d a v e r a g e c o m p r e s s i v e

s t r e s s o f 3,285 p s i , as a l r e a d y n o t e d . I n e a c h c a s e , t h e

v a l u e of t h e modulus i s t h e s l o p e o f t h e c h o r d b e tween

Page 75: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

62.

a) S T R E S S E S D U E TO Pu/z

AAK,. P' S T R E S S CALCULATED F R O M OBSERVATION

STRESS C A L C U L A T E D * U S I N G E f i

S T R E S S CALCULATED* U S I N G Ef

AAK,. P' COMPRESSION TENSION COMPRESSION T E N S I O N WMpRESS IOM T E N D O N

AAK,.

% p 6 i . p s i . p e i . p6>i.

"25 29 31

.23 + 771 + 704 + 663

+ 401 + 404 + 4 8 9

+ 797 + 727 + 670

+ 369 + 379 + 472

+ 806 + 731 + 674

+ 360 + 377 + 464

28 30

. 4 5 + 1 061 + 851

+ 713 + 513

+ 1 078 + 1076

+ 678 + 679

+ 1 083 + 1082

+ 673 + 674

38 39

.60 + 1 341 + 1325

+ 933 + 905

+ 1 347 + 1 360

+ 8 6 8 + 866

+ 1 348 + 1365

+ 865 + 861

36 .91 + 1 692 + 1440 + 1 770 + 1325 4 1774 + 1 320

22 37

1 . 2 0 + -2 2 99 + 2472

+ 1715 + 1512

+ 2 3 4 5 + 2571

+ 1 625 + 1 404

+ 2368 + 2599

+ 1 602 + 1379 I

b) S T R . E S > S E S D I JB TO Pa I

25 29 31

• 23 + 2609 + 2348 + 2609

- 1031 - 852 - 1031

+ 2 9 9 5 + 1838 + 2618

- 1 333 - 1006 - 1042

+ -3084 + 2571 + 2700

- 1 41 9 - 1 079 - 1 1 20

28 30

. 4 5 , + - 3 139 + 2860

- 1461 - 1 200

+ 3509 + 3349

- 1233 - 1 1 09

+ 3648 + 3640

- 1372 - 1210

38 39

.60 + 321 0 + 3533

- 1469 - 1 707

+ 3797 + 4109

- 1072 - 1313

+ 3889 + 4245

- 1 1 71 - 1455

36 .91 + 3945 - 2035 + 4729 - 91 9 + 4820 - 1110

22 37

1 .20 + 4 6 5 5 + 4118

- 2 5 0 5 - 2 1 2 2

+ 6730 + 6675

- 2000 - 1 995

+ 7960 + 7835

~ 3240 - 3165

F H O M S E C A . N J T F O R - M U L A

TABLE I V . - COMPARISON OF STRESSES OBTAINED FROM THE TEST RESULTS WITH THOSE COMPUTED BY BRECKENRIDGE'S MODIFIED SECANT FORMULA

Page 76: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

e * o. i (M ^j- S * OA I N .

e * 0.3 IN.

— e «• 0 . 0 I N . , ,

Sooo 5ooo

6

\oooo psi

(+)

F i g . 1 3/a. C u r v e s o f t h e S e c a n t F o r m u l a P l o t t e d f o r t h e S p e c i m e n s . cn

Page 77: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

P i g . C u r v e s of t h e S e c a n t F o r m u l a P l o t t e d f o r t h e S p e c i m e n s .

Page 78: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

t h e two p o i n t s on t h e c u r v e 855 p s i above and b e l o w t h e

v a l u e o f 3,285 p s i . T h i s i s t h e r a n g e o f a n t i c i p a t e d

s t r e s s e s u n d e r t e s t . A l t h o u g h t h e t e s t r e s u l t s i n

Column 16 showed t h a t t h e a c t u a l a v e r a g e c o m p r e s s i v e

s t r e s s i s 2,960 p s i i n s t e a d o f t h e a n t i c i p a t e d 3,285

p s i t h e r e - e v a l u a t i o n of t h e t e s t r e s u l t s was i g n o r e d .

The m o d u l i so o b t a i n e d a r e shown i n Column 14.

F i g u r e s 14/a and 14/b d e m o n s t r a t e two e x a m p l e s s h o w i n g

t h e above c h o r d as w e l l as t a n g e n t s a t z e r o s t r e s s and

a t 5,700 p s i , w h i c h i s t h e v a l u e of t h e h i g h e s t c o m p r e s s ­

i v e s t r e s s . F i g u r e 14/a i s a r e p r e s e n t a t i v e c y l i n d e r o f

a h i g h q u a l i t y c o n c r e t e w h i l e 14/b i s a r e p r e s e n t a t i v e o f

a l o w e r q u a l i t y .

T a b l e V shows t h e d i f f e r e n t m o d u l i . I n Column 4 a r e

t h e i n i t i a l t a n g e n t m o d u l i w h i c h were e s t a b l i s h e d by

v i s u a l l y f i t t i n g a l i n e a t t h e i n t e r s e c t i o n p o i n t o f t h e

s t r e s s - s t r a i n c u r v e and the a b s c i s s a . S i n c e t h e r e c o r d ­

i n g n e e d l e e x h i b i t e d many i r r e g u l a r i t i e s when the t e s t i n g

s t a r t e d t h e s l o p e of t h e t a n g e n t r e f l e c t s t h e s e u n c e r t a i n ­

t i e s .

Column 1 shows t h e age of t h e c y l i n d e r s . The f i g u r e s

i n t h e p a r e n t h e s i s d e n o t e t h e days of two c y l i n d e r s b r o k e n

a t a d i f f e r e n t t i m e c o r r e s p o n d i n g t o s p e c i m e n s t e s t e d

s e v e r a l d a y s a p a r t . Under t h e h e a d i n g E^, Column 6,

v a l u e s c a l c u l a t e d f r o m t h e b e n d i n g t e s t s a r e t a b u l a t e d .

Column 6 shows t h e v a l u e s - o b t a i n e d f r o m Pauw's 13 i 2r—

e q u a t i o n , E= 33w Jfr now recommended by

Page 79: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

F i g . 14/a. T y p i c a l S t r e s s - s t r a i n C u r v e s f o r C y l i n d e r s .

Page 80: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

fcfcpL-ICA Of T H £ * > T K ^ ^ - ^ T ^ A I M Of

Y

F i g . 14/b. T y p i c a l S t r e s s - s t r a i n C u r v e s f o r C y l i n d e r s .

Page 81: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

68.

I 1 3 4 6 7

T fc Ec MARK- w . IC6I. M. 9-10-11 86 8973 4833' 5256 - 5625 4906

1 2-13-14 1 5-16-17 (104)

77

8777

7652

4683

4017

4953

4480

— 5567

5198

4886

4757 T8-T9 20-21

till) 65

8328 7290

4595 4407

4480 51 50

— 5422

5073 4838 4708

22-23-24 97 6509 3638 4300 : 3960 4794 4590 25-26 96 7087, 4093 4600 4740 5002 4670

27-28-29 96 6448 3685 4202 5100 4771 4579 30-31 - - - - — _

32-33 53 6677 3730 4576 4855 4617 34 64 721 3 4523 4980 5300 5046 4697 35 62 7397 41 1 3 4400 - 5093 4716

36-3^ 38-39 <P>

64

7388 7328

3861 3972

4230 4360

4890 • 4570

5107 5057

4722 4700

TABLE "V... -COMPARISON OF DIFFERENT MODULI

t h e A m e r i c a n and C a n a d i a n Codes, c o r r e s p o n d i n g t o a c t u a l

f ^ ' v a l u e s t a b u l a t e d i n Column 2. A c t u a l d e n s i t y m e a s ure-c ments showed t h a t t h e tpst c y l i n d e r s a v e r a g e d 148 l b s . / c u .

f t . and t h i s v a l u e was u s e d i n t h e c a l c u l a t i o n s .

F o r c o m p a r i s o n p u r p o s e s modulus c a l c u l a t e d f r o m 1 3

J e n s e n ' s f o r m u l a 6x106

J 1 + 2 0 0 0 / f c

a r e shown i n Column 7.

Page 82: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

V I I . DISCUSSION OF TEST RESULTS

I n f l u e n c e o f S t e e l R a t i o on t h e C r i t i c a l Load

The f i r s t q u e s t i o n t o be a n s w e r e d i s w h e t h e r o r n o t

t h e c r i t i c a l l o a d of a p r e s t r e s s e d c o n c r e t e s t r u t depends

on t h e amount o f p r e s t r e s s i n g . F i g u r e 5 shows t h e t e s t

r e s u l t s i n a g r a p h where c r i t i c a l l o a d s , o b t a i n e d f r o m

t h e S o u t h w e l l P l o t s , a r e drawn a g a i n s t the p e r c e n t a g e of

s t e e l . These v a l u e s a r e t h e a v e r a g e s of a l l t e s t r e s u l t s

o b t a i n e d f r o m the s t r u t s w i t h z e r o and 0.3 i n . e c c e n t r i c i ­

t i e s , f o r e a c h s t e e l c o n t e n t . These t e s t r e s u l t s show no

t e n d e n c y o t h e r t h a n t h a t t h e c r i t i c a l ' l o a d does n o t

depend on t h e m a g n i t u d e of p r e s t r e s s i n g . F i g u r e 5 a l s o

shows t h e c o n v e r t e d c r i t i c a l l o a d s w h i c h e l i m i n a t e the

e f f e c t o f t h e v a r i a t i o n i n t h e m o d u l i ( s e e C h a p t e r VI-1 ) .

The p l o t s o f t h e c o n v e r t e d c r i t i c a l l o a d s a l s o l i e a l o n g

a h o r i z o n t a l s t r a i g h t l i n e . I n F i g u r e s 6 and 7 t h e

c r i t i c a l l o a d s ( b o t h t h e a c t u a l and the c o n v e r t e d ) a r e

p l o t t e d s e p a r a t e l y fo.r t h e s t r u t s l o a d e d w i t h z e r o and

0.3 i n . e c c e n t r i c i t i e s . N ote t h a t t h e a v e r a g e of t h e

a c t u a l c r i t i c a l l o a d s f o r t h e c e n t r a l l y l o a d e d s t r u t s

( F i g u r e 6) i s a p p r o x i m a t e l y 23$ h i g h e r t h a n t h a t f o r

s t r u t s w i t h s m a l l e c c e n t r i c i t i e s ( i n F i g u r e 7 ) . C o n v e r t e d

c r i t i c a l v a l u e s i n F i g u r e 6 l i e a l o n g a h o r i z o n t a l l i n e

w h e reas c o n v e r t e d v a l u e s i n F i g u r e 7 a p p e a r t o l i e on a

s l o p i n g l i n e marked A. I f , h o w e v e r , s p e c i m e n No. 27 i s

o m i t t e d f r o m t h i s t a b u l a t i o n p o i n t Y w i l l f a l l a t p o i n t X,

Page 83: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

70.

and t h e n t h e a v e r a g e v a l u e f o r a l l s t r u t s w i l l change

f r o m 45.34 k i p s t o 43.9 k i p s . F o r t h i s c a s e t h e v a l u e s

w i l l come c l o s e r t o a h o r i z o n t a l l i n e . I t i s p o s s i b l e

t h a t s p e c i m e n No. 27 had a h i g h e r v a l u e of t h e m o d u l u s ,

o r h i g h e r p r e s t r e s s , or b o t h , t h a n a n t i c i p a t e d , g i v i n g

an i n o r d i n a t e l y h i g h v a l u e of c r i t i c a l l o a d .

I n C h a p t e r V I - 3 i t was m e n t i o n e d t h a t s o m e t i m e s t h e

l a s t p l o t s f a l l above t h e s t r a i g h t l i n e , an i n d i c a t i o n

t h a t t h e s p e c i m e n a l r e a d y s t a r t e d t o f a i l i n b e n d i n g .

N o t i c e t h e h i g h C J c ^ - ^ t e n s i l e s t r e s s e s of s t r u t s Nos.

24, 15, and 35 i n T a b l e I I I . These t e n s i o n s t r e s s e s a r e

i n t h e r a n g e of the c r a c k i n g l i m i t of t h e c o n c r e t e .

C o n s e q u e n t l y t h e s e s p e c i m e n s m i g h t have c r a c k e d s h o r t l y

b e f o r e t h e i r u l t i m a t e c a p a c i t y was r e a c h e d , and t h e l a s t

p l o t s f e l l a l o n g a h a r d l y n o t i c e a b l e c o n v e x c u r v e r a t h e r

t h a n a l o n g t h e s t r a i g h t l i n e . Thus a p o s s i b l e - e r r o r i n

f i t t i n g t h e s t r a i g h t l i n e may l e a d t o a f a l s e , somewhat

s t e e p e r l i n e g i v i n g a r e s u l t on the low s i d e . The h i g h

v a l u e of s p e c i m e n No. 27 and the l o w e r v a l u e s of s p e c i m e n s

w i t h low . p r e s t r e s s must be c o n s i d e r e d as e x p e r i m e n t a l

e r r o r s , a nd have no b e a r i n g on t h e c o n c l u s i o n t h a t t h e

m a g n i t u d e of t h e E u l e r l o a d o f a p r e s t r e s s e d c o n c r e t e

s t r u t i s i n d e p e n d e n t of t h e amount of p r e s t r e s s .

A p p l i c a b i l i t y of t h e S o u t h w e l l Method

F i g u r e s 1 l / a t o 1 l / f f o r z e r o and 0.3 i n . e c c e n t r i c i t y

show t h a t t h e S o u t h w e l l method of e s t i m a t i n g t h e c r i t i c a l

l o a d s i s r e a s o n a b l y r e l i a b l e f o r p r e s t r e s s e d c o n c r e t e s t r u t s .

Page 84: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

71 .

F i g u r e s 11/g t o 1 1 / i , however i n d i c a t e t h a t f o r

e c c e n t r i c i t i e s o f 1.5 i n . t h e S o u t h w e l l method does n o t

a p p e a r t o he r e l i a b l e .

Of t h e o b s e r v e d v a l u e s , "those g r e a t e r t h a n 7 k i p s f o r

low p r e s t r e s s , and a b o u t 10 k i p s f o r h i g h p r e s t r e s s w i l l

e x c e e d t h e p r o p o r t i o n a l l i m i t , and t h e r e f o r e a r e n o t

u s a b l e . S i m i l a r l y , o b s e r v e d v a l u e s b e l o w a b o u t 4 k i p s

may not have s u f f i c i e n t a c c u r a c y . Thus o n l y a few r e a d ­

i n g s , b e t ween t h e s e l i m i t s , a r e a v a i l a b l e f o r p l o t t i n g ,

and t h e s e do not g i v e a s u f f i c i e n t l y l o n g l i n e t o e s t i m a t e

t h e t r u e c r i t i c a l l o a d .

V a l u e s o f c r i t i c a l l o a d f o r a l l s t r u t s l o a d e d w i t h

z e r o or 0.3 i n . e c c e n t r i c i t y a r e p l o t t e d a g a i n s t v a l u e s

o f a^ w h i c h were o b t a i n e d f r o m t h e S o u t h w e l l P l o t s , i n

F i g u r e 15. T h e r e does n o t a p p e a r t o be any d i s t i n c t

i n d i c a t i o n o f d i f f e r e n c e s i n r e l i a b i l i t y o f t h e method

f o r d i f f e r e n t m a g n i t u d e s of e c c e n t r i c i t y up t o a b o u t

0.3 i n .

The M o d ulus t o be Used

I n o r d e r t o be a b l e t o c a l c u l a t e t h e E u l e r l o a d of

a p r e s t r e s s e d c o n c r e t e s t r u t i t i s n e c e s s a r y t o use t h e

p r o p e r e l a s t i c modulus i n t h e E u l e r f o r m u l a . B e c a u s e t h e

c o n c r e t e m a t e r i a l e x h i b i t s a t l e a s t a s l i g h t c u r v i l i n e a r

r e l a t i o n o f s t r e s s and s t r a i n , e ven a t low v a l u e s , and

i t s p r o p o r t i o n a l l i m i t i s u n d e f i n e d , t h e modulus c o r r e s ­

p o n d i n g t o t h e E u l e r or c r i t i c a l l o a d must be d e f i n e d .

Page 85: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

CONVE&TE.P CRITICAL L0AP£ vs. V A L U E S OF Q \

80

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20

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1 H 1

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•23 27 24 i(b 20 19 10

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3>5 3D> 57 17 OWTC-WT'ONAL) p i g . 15. C o n v e r t e d C r i t i c a l Loads V e r s u s V a l u e s o f

Page 86: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

To i n v e s t i g a t e t h i s p r o b l e m t h e t h e o r e t i c a l c u r v e 2 2

P = Tt E l / I T was drawn i n P i g u r e 16, on a b a s e o f

modulus E. I n F i g u r e 1 6 ( a ) a r e a l s o shown v a l u e s of

P c r . ( f r o m S o u t h w e l l P l o t s ) on a b a s e of t a n g e n t modulus

E^, w h i l e i n F i g u r e 1 6 ( b ) on a b a s e o f i n i t i a l t a n g e n t

modulus E,.. t i

I t a p p e a r s t h a t t h e i n i t i a l t a n g e n t m o d u l i p r o v i d e a

b e t t e r f i t t o t h e t h e o r e t i c a l c u r v e . However, due t o

t h e d i f f i c u l t y i n f i n d i n g t h e i n i t i a l t a n g e n t m o d u l u s ,

i t w o u l d be d e s i r a b l e t o use t h e more e a s i l y o b t a i n e d

s e c a n t modulus of a s t r e s s - s t r a i n c u r v e . C o n s i d e r i n g

t h a t t h e v a l u e s of t h e a v e r a g e c o m p r e s s i v e s t r e s s

of t h e s p e c i m e n s r a n g e b e t w e e n 1,681 p s i and 4,135 p s i ,

i t c a n r e a d i l y be shown t h a t t h e d e v i a t i o n b e t w e e n t h e

s e c a n t m o d u l i c o r r e s p o n d i n g t o t h e s e s t r e s s e s and t h e

t a n g e n t m o d u l i i s n e g l i g i b l e . E x c e p t f o r c y l i n d e r s

No. 22-23-24 and one o f t h e f o u r s t r e s s - s t r a i n c u r v e s of

c y l i n d e r No. 34, a l l s t r e s s - s t r a i n c u r v e s c o r r e s p o n d i n g

t o t h e s p e c i m e n s t e s t e d f o r b u c k l i n g , e x h i b i t e d a c u r v e

v e r y c l o s e t o a s t r a i g h t l i n e i n t h e l o w e r s t r e s s r a n g e

as d e m o n s t r a t e d i n F i g u r e 14/a. C o n s e q u e n t l y t h e s e c a n t

m o d u l i c o r r e s p o n d i n g to' t h e a v e r a g e c o m p r e s s i v e s t r e s s

l e v e l h a r d l y d e v i a t e s f r o m t h e v a l u e s of t h e i n i t i a l

t a n g e n t m o d u l i as s e e n i n F i g u r e 14/a. T h e r e f o r e , c o n ­

s i d e r i n g t h e h i g h s t r e n g t h c o n c r e t e u s e d , t h e i n i t i a l

m odulus c o u l d be r e p l a c e d w i t h good a p p r o x i m a t i o n by t h e

s e c a n t m o d u l u s . S i n c e o n l y two s t r e s s - s t r a i n c u r v e s of

Page 87: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

7 4 .

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MODULUS £

F i g . 16, C o m p a r i s o n o f E u l e r C u r v e w i t h t h e C o n v e r t e d C r i t i c a l L o a d s .

Page 88: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

c y l i n d e r s Wo. 12-13-14 and one of No. 34 showed a

d i v e r g e n c e of and E^ c u r v e s , f u r t h e r r e s e a r c h i s

n eeded t o p r o v e w h e t h e r t h e use of the s e c a n t modulus i n

t h e E u l e r f o r m u l a i s p r o p e r when the s t r u t s a r e made of

low q u a l i t y c o n c r e t e .

P i g u r e 1? shows two commonly u s e d c u r v e s f o r modulus

on a base of c y l i n d e r s t r e n g t h , as w e l l as t h e v a l u e s of

E, and E,. o b t a i n e d f r o m the t e s t c y l i n d e r s . I t a p p e a r s

t h a t b o t h e q u a t i o n s g i v e v a l u e s somewhat i n e x c e s s of

t h e t e s t v a l u e s . Of t h e s e two e q u a t i o n s t h e J e n s e n

e q u a t i o n comes c l o s e r t o t h e d e s i r e d v a l u e s .

U l t i m a t e Load C a r r y i n g C a p a c i t y

A l t h o u g h t h i s r e s e a r c h c o n c e n t r a t e d p r i m a r i l y on t h e

i n v e s t i g a t i o n o f t h e r e l a t i o n s h i p s between t h e E u l e r l o a d

t h e p e r c e n t a g e of s t e e l , and t h e modulus t o be u s e d i n

E u l e r ' s f o r m u l a , a b r i e f d i s c u s s i o n of t h e u l t i m a t e l o a d

c a r r y i n g c a p a c i t y of t h e s p e c i m e n s w o u l d be a p p r o p r i a t e . 2

R e c e n t l y , f o r s t r u t s s u b j e c t t o a x i a l l o a d i n g Brown

d e v e l o p e d an i n e l a s t i c a n a l y t i c a l method t o p r e d i c t t h e

e x t e r n a l u l t i m a t e l o a d P i n t e r m s of t h e s h o r t c o l u m n u

s t r e n g t h and t h e p r e s t r e s s i n g f o r c e F1 c o r r e s p o n d i n g t o S Ul

P , The a n a l y s i s i s b a s e d on t h e f o l l o w i n g p r i n c i p a l ;

1) t h e c r i t i c a l c o n c r e t e c o m p r e s s i v e s t r a i n a t f a i l u r e

i s 8 C = 180 x 1 0 ~ 5 i n . / i n . 2) t h e s t r e s s - s t r a i n r e l a t i o n s h i p f o r c o n c r e t e i s

it t p a r a b o l i c w i t h maximum s t r e s s f = °85f,, o c c u r r i n g >

0 l\ . ^ 11

Page 89: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

76.

F i g . 1 7 . C o m p a r i s o n of Commonly Used C u r v e s of M o dulus w i t h T e s t R e s u l t s .

Page 90: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

where £ = 180 x 1 0 - - 5 i n . / i n . ^ c ' 3) t h e t o t a l d e f l e c t i o n due t o p r e s t r e s s and l o a d i n g

u n d e r c r i t i c a l c o n d i t i o n s i s g i v e n hy = L 2 ^ / 5

where ^ i s a f u n c t i o n o f t h e d e p t h o f t h e s t r e s s

"block a t t h e m i d - p o i n t o f t h e s t r u t .

F o r c e n t r a l l y l o a d e d and c e n t r a l l y p r e s t r e s s e d s t r u t s

Brown f o u n d t h a t t h e summation of t h e e x t e r n a l u l t i m a t e

l o a d P^, and t h e c o r r e s p o n d i n g p r e s t r e s s i n g f o r c e P g u >

i s e q u a l t o t h e s h o r t column s t r e n g t h P = 0 . 8 5 f (A -A ) 0 C C S

m u l t i p l i e d "by a r e d u c t i o n f a c t o r R w h i c h depends on t h e

s l e n d e r n e s s r a t i o and w h i c h i s g i v e n i n g r a p h f o r m i n

h i s p a p e r . Thus P = RP - F ............ e. ) u 0 su

F o r s l e n d e r n e s s r a t i o L / r = 1 3 5 , u s e d i n t h i s t e s t ,

Brown's g r a p h i n d i c a t e s a r e d u c t i o n f a c t o r of R = 0 . 4 7 .

The c a l c u l a t e d r e d u c t i o n f a c t o r s f o r s t r u t s t e s t e d w i t h

z e r o e c c e n t r i c i t y a r e shown i n T a b l e VI'.']- They v a r y

b e t w e e n 0 . 3 4 and 0 . 6 3 .

As l o a d e c c e n t r i c i t y i n c r e a s e s t h e u l t i m a t e l o a d

c a r r y i n g c a p a c i t y d e c r e a s e s . However, whereas r e s u l t s o f

th e s t r u t s t e s t e d w i t h s m a l l ( 0 . 3 i n . ) e c c e n t r i c i t y do no

a p p e a r t o depend on the s t e e l r a t i o ( s e e F i g u r e 1 2 ) , t h e

r e s u l t s o f t h e s t r u t s t e s t e d w i t h l a r g e ( 1 . 5 i n . )

e c c e n t r i c i t y show t h a t t h e i r u l t i m a t e c a p a c i t y i n c r e a s e s

w i t h t h e amount of s t e e l . F i g u r e 18 shows t h e u l t i m a t e

l o a d p l o t t e d a g a i n s t t h e p e r c e n t a g e o f s t e e l b e t w e e n

0 . 2 3 and 1 . 2 0 p e r c e n t .

The e v a l u a t i o n o f P f o r t h e 1 . 5 i n . e c c e n t r i c i t y

Page 91: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

78 .

1. 3. 4- 5. 6. 7 .

M|i.. P . • 8 5 f t Po Pu Pu+Fsu Po

psi. bps kips kips

1 0 1 2

. 2 3 7630 7460

1 83 179

7 .2 7 .2

66 .0 54 .2

»40 .34

1 8 21

.45 7080 6200

1 69 1 48

13.6 13 .7

58 .9 48 .4

.43

.42 1 1 H

.60 7630 7460

1 82 1 78

17 .9 18.1

65 .0 57 .5

.46

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9 1 3 • 34 36

.91 7630 7630 61 40 6280

1 81 1 81 1 46 149

27 .2 26 .6 27 .2 2 7 . 0

62 . 5 72 .5 57 .2 54 .2

.50

.55

.58

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1 9 20 37

1 .20 7080 6200 6280

1 68 1 47 1 49

35 .7 35 .4 36.6

60 .0 57 .9 43 .6

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.54

TABLE V I . - REDUCTION FACTORS FOR STRUTS

WITH ZERO ECCENTRICITY.

needs i n e l a s t i c a n a l y s i s , which i s beyond the scope of

t h i s t h e s i s . However, at a r b i t r a r i l y chosen loads of

P /2 the behaviour of the s t r u t s i s e l a s t i c . At these u

loads the te s t s show c lo se agreement with the s t r e s s e s

c a l c u l a t e d from the mod i f ied secant formula (as shown i n

Table IV /a ) , i n d i c a t i n g 'the v a l i d i t y of i t s use w i t h i n

the' p r o p o r t i o n a l l i m i t .

Page 92: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

ULTIAAATLt Lc9AD (Pu) V4. p %

F i g . 18. U l t i m a t e Load o f S t r u t s w i t h 1 .5 i n . E c c e n t r i c i t y V e r s u s S t e e l R a t i o .

Page 93: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

CONCLUSIONS

The E u l e r l o a d of a s l e n d e r p r e s t r e s s e d c o n c r e t e s t r u t

does n o t depend on t h e amount of p r e s t r e s s i n g f o r c e

p r o v i d e d t h a t 1) t h e s t r e s s due t o t h e p r e s t r e s s i n g i s

l e s s t h a n t h e c r i t i c a l s t r e s s and 2) t h e c o n c r e t e i s

of s u c h a q u a l i t y as t o f o l l o w Hooke's Law. Under t h e s e

c o n d i t i o n s t h e b u c k l i n g l o a d c a n be c a l c u l a t e d by E u l e r ' s

f u n d a m e n t a l f o r m u l a .

The method o f t h e S o u t h w e l l P l o t may be u s e d t o f i n d the

c r i t i c a l l o a d f o r p r e s t r e s s e d c o n c r e t e s t r u t s . E c c e n t r i ­

c i t y r a t i o e / t = .1 does n o t i n t r o d u c e any s u b s t a n t i a l

e r r o r .

S e c a n t m o d u l u s , o b t a i n e d f r o m s t a n d a r d c o n t r o l c y l i n d e r s ,

w i l l y i e l d r e a s o n a b l y good v a l u e s of t h e b u c k l i n g l o a d .

When th e u l t i m a t e c a p a c i t y of a p r e s t r e s s e d c o n c r e t e

s t r u t ( h a v i n g a s t e e l r a t i o l e s s t h a n 1.2%) i s g o v e r n e d

by b e n d i n g r a t h e r t h a n by b u c k l i n g , i t s c a p a c i t y i s

p r o p o r t i o n a l t o t h e m a g n i t u d e of p r e s t r e s s .

I n s p i t e o f t h e c a r e t a k e n i n t h e p r e p a r a t i o n o f t h e

s p e c i m e n s , and i n t h e l o a d i n g p r o c e d u r e s , t h e d i f f e r e n t

t e s t r e s u l t s show c o n s i d e r a b l e s p r e a d .

Page 94: EXPERIMENTAL RESEARC OHN THE BUCKLIN'G BEHAVIOUR OF ...

81 .

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7. J e n s en, V. P. , The E l a s t i c i t y R a t i o o f C o n c r e t e and i t s

E f f e c t on t h e U l t i m a t e S t r e n g t h o f Beams, A. C. I . J o u r n a l

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9. L i n , T. Y. and I t a y a . R.. A P r e s t r e s s e d C o n c r e t e Column

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C o n c r e t e I n s t i t u t e , V o l . 2, No. 3 Dec. 1957.

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B e h a v i o u r of P r e s t r e s s e d C o n c r e t e Columns, Techn. P r o g r e s s i

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11. Osgood, ¥. R., The D o u b l e Modulus T h e o r y of Column A c t i o n .

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C o n c r e t e Columns, T e c h n . P a p e r S e r i e s No. 131 Eng. P r o g r e s s

a t t h e U n i v e r s i t y of F l o r i d a V o l . X I No. 7 J u l y 1957.