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Rationale for Simplifying the Strength Formulae
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Rationale for Simplifying the Strength Formulae for the Design of Multi-row Bolted Connections
Failing in Net TensionFailing in Net Tension
Toby Mottram DSc, FIStructE, CEngToby Mottram DSc, FIStructE, CEng Civil Research Group, School of Engineering, Warwick University
ACIC 2013 Q een’s Uni ersit of BelfastQueen’s University of Belfast
10th - 12th September 2013
Pultruded FRP Shapes Pultruded FRP Shapes –– ASCE StandardASCE Standard“Standard for Load and Resistance Factor Design (LRFD) of Pultruded
22
Fiber-Reinforced Polymer (FRP) Structures”Simple non-sway frames with bracing.
Beam-to-column web-cleated connection
from Strongwell Design Manual
For buildings to three storeys of height.
CHAPTERS:
Pultruded FRP Shapes Pultruded FRP Shapes –– ASCE StandardASCE Standard 33
1. General Provisions
2. Design Requirements
3. Tension Members
4. Design of Compression Members
5. Design for Flexure and Shear
6. Members Under Combined Forces
and Torsion
7. Plates and Built-up Members
8 BOLTED CONNECTIONS8. BOLTED CONNECTIONS.Project to write draft 2008-10.
Published in 2014.
Note that in the USA the word connection is our word joint, and vice versa.
ASCE Standard ASCE Standard –– Net Tension StrengthNet Tension StrengthNet tension resistance of a double lap shear
44
pconnection with multi-rows of bolts
se1 s
pitch distanceend distance
e2
dn Direction
side distance
g of pultrusion
Tensile load
Tensile load gage distance
Tensile load
Tensile load
t plate thickness
Bolts of diameter d (< dn) are not shown
First bolt row for inner plate of thickness t
Testing often has outer plates of steel (ASTM and EN standards).
ASCE Standard ASCE Standard –– Net tension Strength Net tension Strength Net-tension failure for connections with two rows of bolts
55
Tension load
Damage Failure
First bolt row = 0
Ultimate Load
gLoad
load
Tension load
St kTe
nsile
Sources: PhD theses C Lutz (2005) & P Wang (2004)
Stroke
For this failure mode the damage and ultimate loads can be the same.
Sources: PhD theses, C. Lutz (2005) & P. Wang (2004)
Net-tension failure for connections with two rows of bolts
66ASCE Standard ASCE Standard –– Net tension Strength Net tension Strength
Locations for stress concentrations causing failurePeak stresses are at points A
d ‘Linear elastic’
causing failure Peak stresses are at points A
ensi
le lo
ad Linear elastic response to
rupture Tension load
Stroke
Te
Source: PhD thesis, P. Wang (2004)
Assumed net-tension failure plane for
resistance model
Model for net-tension resistance, this is Rnt f
77ASCE Standard ASCE Standard –– Net tension Strength Net tension Strength
w = 2e2
, nt,f
(1-Lbr) Rnt,f/2e1
Tension stress due to LbrRnt,f
Peak stress at h l d t
(1-Lbr) Rnt,f/2 Tension stress due to (1-Lbr)Rnt,f
Peak stress at h l d t
Row 2
Filled-hole Open-hole
LbrRnt,f/2
dn
d hole due to bearing load
stress at
LbrRnt,f/2A
stress at
hole due to bypass load
s =
4d m
in.
Row 1n t
A
free edge
Hole centre
d
A
stress at free edge
Hole centre
R
t
R
Net-tension failure plane
Rnt,f Rnt,f
Semi-empirical model by Hart-Smith (1987)
88ASCE Standard ASCE Standard –– Net tension Strength Net tension Strength
Term in brackets is a reduction factor
w is width
tLnt,f
1 FtwR
t is thickness
d is bolt diameter
d i h l di t brLop,
brLnt,
,
1
1
wd
LKdwLK
n
dn is hole diameter
Lbr proportion of tension load taken in bearing by first bolt row (steel
d FRP L 0 6 (?))w and FRP Lbr = 0.6 (?))
is Longitudinal tensile strength of the pultruded material.tLF
Knt,L depends on geometry and a filled-hole correlation coefficient (CL).
Kop,L depends on geometry and an open-hole correlation coefficient (Cop,L).
Model for case when loading direction and orientation of pultruded material are aligned ( = 0).
Evaluation of semi-empirical model by Hart-Smith (1987)
99ASCE Standard ASCE Standard –– Net tension Strength Net tension Strength
Not time to discuss all issues for evaluation!!
Open hole correlation coefficient, Cop L0.8
Open hole correlation coefficient, Cop,L
11
opte
tcLop,
kkC
3n
opte, 12
wdk
= 0.374 (mean), CoV 23.5%is the isotropic stress concentration factor.
ktc is the orthotropic stress
0.6
ktc -
1
1opte,k
tc pconcentration determined by experiment using open hole specimens with
0.4
k
Not linear relationship!
different dn/w ratios.0.2
1.0 1.2 1.4 1.6
kte op -1
Different material!
kte,op 1
Test results from G. J. Turvey and P. Wang, 'Open-hole strength of pultruded plate,' Structures & Buildings, 156 1, 2003, 93-101.
Net-tension failure for connections with two rows of bolts.
1010ASCE Standard ASCE Standard –– Net tension Strength Net tension Strength
Plotted Longitudinal connection results required three studies.
RT with as received material
1.20
1.40 Each test number is for a different connection geometry, having
RT with as-received material
0 60
0.80
1.00
exp/R
nf,f,
theo
ry
g y, gconstant bolt diameter and type, plate thickness and tightening CL = 0.33 (bearing); Cop,L = 0.37 (by-pass);
0.20
0.40
0.60
Rnf
,f,e
torque.
Resistance ratios are
t = 12.7 mm; d = 19.05 mm; dn = 20.6 mm;
= 166 N/mm2 (mean); torque is 32.5 N.mtLF
0.000 2 4 6 8 10 12
Test Number
Resistance ratios are for conservative design.
J . T. Mottram, ‘Prediction of net–tension strength for multi-rowed boltedconnections of pultruded material using the Hart-Smith semi-empiricalmodeling approach,’ Composites for Construction, (14)1, (2010),105-114.
Findings from evaluation exercise:
1111ASCE Standard ASCE Standard –– Net tension Strength Net tension Strength
Findings from evaluation exercise:
• Comparison between experimental and predicted strengths for 17 differentconnection geometries show that the simple modelling approach has potentialto give safe and reliable net-tension strength predictions.
• For the two connections that did not give a safe prediction it is observed thattheir same geometry would not be designed for.g y g
Practitioners on the ASCE/SEI Fiber Composites And Polymers Standardscommittee (FCAPS), said that they would NOT use the Hart-Smith designmethod as it is too complicated.p
Resolution Resolution –– Net tension MultiNet tension Multi--bolt Rowsbolt Rows 1212
Rnf,t = rf w t tLF
1
1
LKwLKrf brLop,brLnt
1Equ. (3)
wdnnd
LKrfn
brLnt,
1q ( )
rf is reduction factor to gross cross-sectional strength
What is the range for rf for connection details permitted by the ASCEWhat is the range for rf for connection details permitted by the ASCEstandard?
The minimum value will provide a simple formula for practitioners to use.
Minimum requirements for bolted connection geometries for multi-row
Resolution Resolution –– Net tension MultiNet tension Multi--bolt Rowsbolt Rows 1313
Minimum requirements for bolted connection geometries for multi row configurations without bolt stagger
Notation Definition Minimum required spacing (or distance in terms of nominal bolt diameters)
Tension or compression load
e1,min End distance 2de2,min Edge distance 1.5d
s = 40e = 20N
smin Pitch spacing 4dgmin Gage spacing 4d
e2 = 15
s = 40e1 = 20 d = 10 & dn = 11.6
70
g =
40 First bolt row
LL Connection force
T
Resolution Resolution –– Net tension MultiNet tension Multi--bolt Rowsbolt Rows 1414
Many geometries are NOT simple plate-to-plate connections.
Values of the reduction factor (rf) from Equ. (3) for the multi-row configuration
Resolution Resolution –– Net tension MultiNet tension Multi--bolt Rowsbolt Rows 1515
e2/d g/d w/d rf
1 5 4 7 0 34
( ) q ( ) gof two rows of two bolts per row illustrated.
1.5 4 7 0.34
1.5 8 11 0.26
1.5 12 15 0.20 smallest rf3 4 10 0.38
4 4 12 0.39
Resolution Resolution –– Net tension MultiNet tension Multi--bolt Rowsbolt Rows 1616
• An EXCEL spreadsheet can be used to apply the Hart-Smith formulae (andaccompanying design parameters).
A l ti l t i t d ll d ti t i l f l• An analytical parametric study allows reduction to a single formula.
• It is .
• This lower bound strength is for the range of connections that are practical and
Rnf,t = 0.2 w t tLF
• This lower bound strength is for the range of connections that are practical andpermitted in the LRFD standard to be published by ASCE. (It is not known ifthe geometry for reduction factor 0.2 provides the net tension mode of failure.)
B th l b d t th b h lf th t l d i t th th• Because the lower bound strength can be half the actual design strength thefull set of formulae are made available in an appendix with the commentary.
• When applying the ‘simplified’ formula it is to be recognize that there can be amaximum limit on the effective (or actual) width (w) of the connectedcomponent for the strength Rnf,t to be valid.
J. T. Mottram 2013