lllllDlll IIIIIIII NE flll lltwo-dimensional state of stress that occurs in thin-walled piping...
Transcript of lllllDlll IIIIIIII NE flll lltwo-dimensional state of stress that occurs in thin-walled piping...
AD-AIl12 050 DAVID W TAYLOR NAVAL SHIP RESEARCH AND DEVELOPMENT CE--ETC F/B 13/11 STRESS INDICES AND FLEXIBILITY FACTORS FOR 90-DEGREE PIPING ELB-ETC(U)FEB 82 A J QUEZON, G C EVERSTINE
UNCLASSIFIED OTNSROC/CMLD DC2/05 NL
NE flll ll....fE° hIhEEEEliI/IlllllDlll
IIIIIIII
1.00
i 11111L.8
l 1II.25 I
MR- , • nil I I I H R I I
C4 DAVID W. TAYLOR NAVAL SHIPRESEARCH AND DEVELOPMENT CENTER0
U Bethesda, Maryand 20084
STRESS INDICES AND FLEXIBILITY FACTORS FOR
90-DEGREE PIPING ELBOWS WITH STRAIGHT PIPE
EXTENS IONS
cn by
oA. J. Quezon and G. C. Everstine
a% APPROVED FOR PUBLIC RELEASE: DISTRIBUTION UNLIMITED.
w~ H COMPUTATION, MATHEMATICS,* AND LOGISTICS DEPARTMENT
DEPARTMENTAL REPORTLoJ
'.j U2
February 1982 DTNSRDC/CMLD-82 /05iI D-
NOWMNAD 50210 2-0)82 0 k 67(gupersedes 3000146)
MAJOR DTNSRDC ORGANIZATIONAL COMPONENTS
DTN3RD)C
COMMANDER 0TECHNICAL DIRECTOR
01
OFFICER-IN-CHARGE OFFICER-IN-CHARGECARDEROCK 05ANNAPOLIS 0
SYSTEMSDEVELOPMENTDEPARTMENT
SHIP ERFORANCEAVIATION ANDSHIPPERORMNCE ______SURFACE EFFECTS
DEPARTMENT DEPARTMENT15 16
STRUCTURES COMPUTATION,DEPARMENTMATHEMATICS AND
DEPARMENTLOGISTICS DEPARTMENT17 18
SHIPACOUTIC PROPULSION ANDSHPACOT ICSNT AUXILIARY SYSTEMS
DEARMET 19 ( DEPARTMENT 27
SHIP MATERIALS ________CENTRAL
ENGINEERING INSTRUMENTATIONDEPARTMENT I DEPARTMENT 1
__ _28___ 29
GPO 866 993 NDW-OTNSROC 3W0/43 INOV 2-W
UNCLASSIFIED.ECU ,ITY CLASSIFICATION OF THIS PAGE (When Date Entered)
READ INSTRUCTIONSREPORT DOCUMENTATION PAGE BEFORE COMPLETING FORM1, REPORT NUMBER 2. GOVT ACCESSION NO. 3. RECIPIENT'S CATALOG NUMBER
4. TITLE (nd Subtitle) 5. TYPE OF REPORT & PERIOD COVERED~STRESS INDICES AND FLEXIBILITY FACTORS FOR90-DEGREE PIPING ELBOWS WITH STRAIGHT PIPE
EXTENSIONS 6. PERFORMING OrG. REPORT NUMBER =
7. AUTHOR(e S. CONTRACT OR GRANT NUMBER(e)
A. J. Quezon and G. C. Everstine
9. PERFORMING ORGANIZATION NAME AND ADDRESS 10. PROGRAM ELEMENT. PROJECT. TASKAREA A WORK UNIT NUMBERSDavid W. Taylor Naval Ship Research Program Element 63561N
and Development Center Task Area S0348001Bethesda, Maryland 20084 Work Unit 1-2740-163
11. CONTROLLING OFFICE NAME AND ADDRESS 12. REPORT DATE
February 19821S. NUMBER OF PAGES
14. MONITORING AGENCY NAME a AODRESS(II different from Controlling Office) IS. SECURITY CLASS. (of this report)
UNCLASSIFIED
ISa. DECL ASSI FIC ATION/DOWN GRADINGSCHEDULE
16. DISTRIBUTION STATEMENT (of this Report)
APPROVED FOR PUBLIC RELEASE: DISTRIBUTION UNLIMITED
17. DISTRIBUTION STATEMENT (of the abstract entered In Block 20, If different from Report)
IS, SUPPLEMENTARY NOTES
19. KEY WORDS (Continue on reverse elde If neceeeary and Identify by bloc, number)
Piping Finite Element Flexibility FactorElbow NASTRANBend Stress Index
20. AESrACT (Continue en reveree eide if neceemay end IdentIfy by block number)
A finite element parameter study ,ms performed on a wide variety of90-degree piping elbows having straight pipe extensions to determine thesensitivity of stress indices and flexibility factors to the length of thepipe extensions. Both moment and force loadings were considered. It wasfound that stress indices are generally insensitive to the type of load(moment or force). Flexibility factors are sensitive to load type only
(Continued on reverse side)
DO . 1473 EDITION OF I NOV 66 1 OBSOLETE UNCLASSIFIEDS/N 0102-LF-014-6601
SECURITY CLAUIFICAION OF THII PAGE (Sie. Det Shtee.E)
SECURITY CLASSIFICATION OF THIS PACE (When Does Sat* .*)
(Block 20 continued)
for short pipe extensions. Flexibility factors for moments generally exceedthose for forces. Stress indices are sensitive to length of pipe extensiononly for A< 0.35, where X is the bend characteristic parameter. Flexibilityfactors are sensitive to length of pipe extension over the entire range ofelbow parameters considered. The "critical length" of straight pipeextension (defined as the minimum length of pipe for which the elbow stressindex is insensitive to further increases in pipe length) was found to beabout three pipe diameters for A< 0.35 and one diameter for A>0.35. Acomparison of the finite element results to those of a torus program calledELBOW indicated that ELBOW is generally not adequate for predicting stressindices and flexibility factors for 90-degree elbows with straight pipe
a r
r r
o C A .....
.~/o
UNCLASSIFIEDSECURITY CLASSIFICATION OF THIS PAELE'Uhm DaM SMtm1i0
limb
TABLE OF CONTENTS
Page
LIST OF FIGURES . . . . . . ................................... iii ***** j
ADISTR ATIVESIFRMO ...... ............................... .. . .. 1v
ASOPET OF ....STUDY......................... ......... ... .. . ... .... 6
APPROSACH V INOMAIN............................. 1
PNTSONTATION AND........ DICSSO OF ..RESULTS..........15..
CEFNLUIONS ......................................... 19
RCOENDATIONSY... o.......... oo .. .... .. .o ... -... o.... o....24
APPROACH oT........... .oo........ -........ .. .o . . .. o . .. ... o....25
APPENDIX - TABLES OF FINITE ELEMENT RESULTS FOR 90-DEGREE ELBOWSWITH STRAIGHT PIPE EXTENSIONS .... .o........... ... 27
REFERENCES ...... ..... o.. .o.. ~o...... o........... o.... ...... 51.
LIST OF FIGURES
I - Pictorial Representation of Nondimensional Elbow Geometric Data .... 9
2 - Geometry and Configuration of Piping Elbow .. oo... o.... ......... 12
3 - Typical Finite Element Model of Piping Elbow o.o.oo..... .o..o...... 14
4 - Sensitivity of Stress Index to Length of Pipe Extension ... oo..... 17
5 - Sensitivity of Flexibility Factors to Length of Pipe
6 - Sensitivity of Flexibility Factors to Length of Pipe
Ex e s ost/ .4 . o ~ o o o.. . . o o ~ . o o o . * o. . 2
LIST OF FIGURES (Continued)
Page
7 - Comparison of Finite Element and ELBOW Flexibility Factors ......... 23
LIST OF TABLES
1 - Dimensions of Piping Elbows ........................................ 7
2 - Nondimensional Elbow Geometric Data ................................ 8
3 - Stress Indices For Elbows Having Equal Length StraightPipe Extensions of Length Three Diameters .......................... 18
4 - Flexibility Factors for Elbows Having Equal Length StraightPipe Extensions of Length Three Diameters .......................... 22
iv
ABSTRACT
A finite element parameter study was performed ona wide variety of 90-degree piping elbows havingstraight pipe extensions to determine the sensitivityof stress indices and flexibility factors to thelength of the pipe extensions. Both moment and forceloadings were considered. It was found that stressindices are generally insensitive to the type of load(moment or force). Flexibility factors are sensitiveto load type only for short pipe extensions.Flexibility factors for moments generally exceed thosefor forces. Stress indices are sensitive to length of
pipe extension only for X < 0.35, where X is the bendcharacteristic parameter. Flexibility factors aresensitive to length of pipe extension over the entirerange of elbow parameters considered. The "criticallength" of straight pipe extension (defined as theminimum length of pipe for which the elbow stressindex is insensitive to further increases in pipelength) was found to be about three pipe diameters forX < 0.35 and one diameter for X > 0.35. A comparisonof the finite element results to those of a torusprogram called ELBOW indicated that ELBOW is generallynot adequate for predicting stress indices andflexibility factors for 90-degree elbows with straightpipe extensions.
ADMINISTRATIVE INFORMATION
This work was sponsored by the Naval Sea Systems Command in Program
Element/Task Area 63561N/S0348001, Task 21302, Work Unit 1-2740-163.
Naval Sea Systems Command cognizant program manager is Dr. F. Ventriglio
(NAVSEA 05R).
INTRODUCTION
Common practice in the design of shipboard piping systems is to
compute stresses and flexibilities for piping elbows using elementary beam
theory for straight beams and applying correction factors called stress
no,1
indices and flexibility factors. The correction factors are generally
calculated by assuming that the elbow behaves as if it were part of a complete
torus, for which analytical solutions for stresses and flexibilities are
available. This approach thus accounts for the bend radius, the pipe
diameter, the wall thickness, the material properties, and the internal
pressure (a nonlinear effect when combined with other loads). However,
the approach ignores such considerations as the bend angle and end
conditions, which can include flanges, straight pipe extensions, or other
elbows.
Since the inclusion of these considerations rules out the use of analytic
solutions, the only way to compute stresses and flexibilities in such cases
is to use an approximate numerical approach such as the finite element method.
The finite element method is well-established in general and has, in
particular, been verified as suitable for predicting the static behavior of
piping elbows and tees [1-3i.
The overall aim of this work is to determine the flexibilities and
stresses in piping elbows and bends in the configurations commonly used on
naval ships. This report addresses in particular the end condition proilem
by analyzing in some detail 90-degree elbows with straight pipe extensions
of various 'Fngths.
The general approach is to analyze a selection of elbows of a variety
sufficient (1) to determine the sensitivity of the elbow stress indices and
flexibility factors to the length of straight pipe extensions, and (2) to
determine the minimum length of straight pipe extension (Lhe "critical
length") for which the stress indices are considered insensitive to further
increases in pipe length.
* A complete listing of references is given on page 51.
2
The volume of data generated by these analyses is sufficiently complex
that only preliminary conclusions will be drawn from the data at this time.
A follow-up report will present a more complete analysis of the data presented
here and develop usable design equations, formulas, or curves.
DEFINITIONS
The stress index c for an elbow is defined [4,5] as the ratio of the
maximum stress intensity for the elbow to the maximum bending stress in a
straight pipe having the same cross section. The stress intensity S is
defined as twice the maximum shear stress in the elbow for a given loading
condition. Thus the maximum stress intensity is the maximum of
s: = 11 - 21 = {(a- a )z + 4T2}Ix y XY
s2 - 1l - 031 = I(G. + Gy) + S 1/2S3 = 102 - 031 = I(ax + Gy) - S1[12
for any arbitrary orientation of an applied moment vector M, where, for the
two-dimensional state of stress that occurs in thin-walled piping elbows,
0, = maximum principal stress
02 = minimum principal stress
03 = 0 (the third principal stress in 3-D elasticity)
x, c a normal stresses in longitudinal and circumferential directions
T - shear stressxy
The calculation of Smax (the maximum of S1, $29 and S3) requires a search
over all possible orientations of the moment vector M. Hence, the stress
index c is given by
3t
max /no m (2)
where a is the nominal stress for the corresponding straight pipe asnom
predicted by elementary beam theory:
0 = M/Z (3)nora
where Z is the section modulus.
For internal pressure loading,
c= max/nom (4)
where a is the maximum stress in the elbow subjected to internal pressure.max
The nominal stress a is taken as the maximum stress occurring in anom
cylindrical pressure vessel due to an internal pressure load:
o nm =pr/t (5)nom, f
where p is the applied internal pressure, r is the mean pipe radius, and t is
the wall thickness.
The flexibility factor k for a piping component (e.g., an elbow) is
defined as the ratio of a relative rotation of that component to a nominal
rotation:
k 6 ab /nom (6)
where eab rotation of end "a" of the piping component relative to end "b"
of that component due to a moment loading M, and in the direction
of M
0nom A nak rotation of an equal length of straight pipe due to the
moment M
4!
For elbows, the nominal rotation is computed using beam theory, in which case
e no .- ML/EI (7)norm
for inplane and out-of-plane moments, and
eo- ML/GJ (8)nom
for torsional moments, where
M - applied moment load
L = arc length of centerline of elbow
E - Young's modulus of material
G = shear modulus of material
I = moment of inertia of cross section
J = torsional constant of cross section kequal to the polar moment of
inertia for circular cross sections)
For 90-degree elbows, L=TR/2 , where R is the bend radius.
The critical length of pipe extension for an elbow is defined here as the
minimum length of straight pipe extension for which the stress index is
considered insensitive to further increases in pipe length. This
sensitivity results from the reduced ability of the elbow to ovalize due
to the presence of straight pipes and flanges. At some length of pipe
extension (the critical length), additional end effects due to the restriction
of ovalization no longer occur.
The bend characteristic parameter X, a dimensionless parameter widely
used in elbow design, is defined as
- tR/r2 1V-2 (9)
5
where t - wall thickness
R - bend radius
r - mean pipe radius
V - Poisson's ratio of material
The nondimensional bend radius Y is defined as
y - R/r (10)
The internal pressure loading parameter i is defined as
= pR2 /Ert (11)
where p is the internal pressure.
SCOPE OF STUDY
Table I summarizes the piping elbows of interest to naval piping
designers. (The data in this table were compiled by Mr. L.M. Kaldor of the
Machinery Stress Analysis Branch (Code 2744) of the David W. Taylor Naval Ship
R&D Center, Annapolis, Maryland.) Included are elbows of 19 nominal pipe
sizes, four bend radii, and three materials. The data in the table represent
a total of 204 different elbows, a number which must be reduced if the
parameter study is to be reasonably manageable.
The information in Table 1 can also be displayed in nondimensional form
Table 2) by dividing all length dimensions by the mean pipe radius r for each
elbow. A graphical display is more useful still. Since the two key
geometrical parameters defining an elbow are its nondimensional wall thickness
and bend radius, we can use these two parameters to construct a figure (Figure
1) which locates all elbows of interest. In Figure 1, a dot is entered for
6
TABLE 1 - DIMENSIONS OF PIPING ELBOWS
Nominal Min. Wall Thickness (in.) Bend Radius (in.)Pipe Outside -
Size Diameter CA715 CA719 In625 SR LR 3D 5D(NPS) (in.) 700 psi 1050 psi 1050 psi
1/4 .540 .065 .106 .012* - - - 1.253/8 .675 .072 .110 .014* - 1.8751/2 .840 .072 .115 .018* - 1.5 1.5 2.53/4 1.050 .083 .121 .022* - 1.125 2.25 3.75
1 1.315 .095 .129 .028* 1 1.5 3 51 1/4 1.660 .095 .139 .035* 1.25 1.875 3.75 6.251 1/2 1.900 .109 .146 .040* 1.5 2.25 4.5 7.52 2.375 .120 .160 .050* 2 3 6 102 1/2 2.875 .134 .175 .060* 2.5 3.75 7.5 12.53 3.500 .165 .193 .073 3 4.5 9 153 1/2 4.000 .180 .208 .083 3.5 5.25 10.5 17.54 4.500 .203 .222 .093 4 6 12 205 5.563 .220 .253 .115 5 7.5 15 256 6.625 .259 .285 .137 6 9 18 308 8.625 .340 .343 .179 8 12 24 4010 10.750 .380 .405 .223 10 15 30 5012 12.750 .454 .464 .264 12 18 36 6014 14.000 .473 .501 .290 14 21 42 7016 16.000 .534 .559 .331 16 24 48 80
Poisson's ratio .294 .294 .309Young's modulus 22.E6 22.E6 30.E6 psi
* Thickness may be greater due to welding considerations.
.. . ..... 7
o n o 000 7 D00 Ac -0
Lrrr W) o r r-SQ
Un diL)L)L) r f LN ) Lr) Ln o S
-~ -~ - -- C1
O ~ ~ C Cfl C-- - W-.4- --
- C)1 1
W) -r-SQr-- N : N O VI
.Vr O 1 - -
L) 4-ow4 Y D v - 0 L
0 .-j z.
0I Ln CU r
.l 40 0 -- %-T0 f %al -l I-.T. 1 - o rr 010 l 0 a
z - - --- -41 1
CU tl M CMM M M ( C4C4C4 C
I- I0 00 ON 00 n% It0P n0M c' IC
-44
c-o '- m coc , 10a
0 col C4 N - - - - -- -- N 0
- - -? - N N'o 0 ) N N' -r )-0 -. 4 t- -4 4 -4 I-. 9
m ., r, 00 - m 00 0000c00 C.4- 0: .; 4 L '
. . . 4 C 4 A4 4- ~ 00C4I ?0jC4 0
o qNe TL CU 0N0 0 0 0 0CC0 4
00
'4 0 0u
P4
,4 -4/ od
-44
0q 0.0 ,0
-4,
U) /) II
r4.4
-4-4
0
C;
P4 -a - U-4 -
co -t o
(a/V -k nTPV PuO TguTBU(T'u0
each of the 204 elbows in Tables I and 2. The figure is useful because it
indicates the ranges of interest for the geometrical parameters t/r and R/r.
The collection of dots in Figure I has also been enclosed by a dashed
polygon. We expect that the range of behavior (stresses and flexibilities) of
elbows can be deduced by studying primarily elbows lying on the periphery of
the polygon. Moreover, the elbows actually analyzed would not have to be real
elbows appearing in Tables 1 and 2, but merely a suitable collection of elbows
defined by parameter pairs (t/r and R/r) lying on the polygon in Figure 1.
Also shown in Figure I are several curves of constant X, the bend
characteristic parameter, assuming a Poisson's ratio of 0.3, which is typical
for the materials listed in Table 1. These curves are useful fcr observing
the range of X represented by the elbows in Table I and for verifying the
extent to which certain elbow behavior depends only on A, as predicted by the
idealized theory for tori.
This study will therefore concentrate on elbows defined by the periphery
of the polygon in Figure 1. In addition, only 90-degree elbows with straight
pipe extensions will be considered. Elbows with other bend angles and end
conditions will be studied in future efforts.
For moment and force loadings, the internal pressure in the pipe is
assumed to be zero throughout this report. To assume otherwise introduces
a nonlinear effect which would greatly complicate the analyses. However,
because the nonzero pressure case is of considerable interest, it will be
pursued in future work.
APPROACH
Elbows defined by the parameter pairs t/r and R/r were chosen primarily
10
from the periphery of the polygon in Figure 1. For each elbow chosen, finite
element analyses were performed by the NASTRAN structural analysis computer
program in order to compute flexibility factors and stress indices for various
lengths of straight pipe extension varying from near zero to three or four
pipe diameters.
The elbow configuration modeled consists of a 90-degree elbow with
straight pipe extensions attached to each end of the elbow, as shown in Figure
2. The end of one pipe extension was fixed. The end of the other pipe
extension was terminated with a rigid flange. Applied loads consisted of
internal pressure as well as the six possible forces and moments applied to
the flange at the free end. For this study, internal pressure loads are not
combined with either force or moment loads.
The finite element results were also compared to results obtained by a
fast-running computer program called ELBOW (61 which is used by some piping
designers. Program ELBOW uses analytical methods to compute flexibility
factors and stress indices for elbows idealized as endless toroidal sections.
For zero internal pressure (ip=0), ELBOW's calculation of the flexibility
factor depends only on the bend characteristic parameter A.
For flexibility factors only, the finite element results were also
compared to flexibility factors computed according to the current ASME code
[71, which, for zero internal pressure, uses the relation
k = 1.65/h (12)
where
h - tR/r2 (13)
and a k calculated to be less than unity is taken as unity.
11
(i IiCiC:
0
4) Cho
'-44
00
12
For internal pressure loading, the finite element results for the stress
index c were also compared to the frequently used analytical expression
c = (2y - 1)/(2y - 2) (14)
presented in the Kellogg book [51, where Y is the nondimensional bend radius
(R/r). Since for our elbows Y ranges from about 1.5 to 11, Equation (14)
indicates that the internal pressure stress index should be between I and 2.
A typical finite element model of an elbow and the two straight pipe
extensions is shown in Figure 3. By symmetry, only half of the circumference
of the elbow cross section need be modeled. The elbow and pipe extensions
were modeled using NASTRAN's two-dimensional quadrilateral QUAD2 plate element
with aspect ratios averaging near unity in the elbow region and about two near
the ends of the pipe extensions. All models used 12 elements in the
circumferential direction.
To compute flexibility factors, the average rotations of the cross
sections at each end of the elbow were required. These averages were obtained
in each cross section of interest by defining in that cross section an
imaginary center point which was connected to the points on the circumference
by beam elements flexible enough not to contribute significantly to the
stiffness of the model.
A special purpose finite element data generator was written to automate
completely the preparation of the NASTRAN input data decks so that the
specification of only a few parameters was required to analyze a particular
case.
Poisson's ratio was fixed at 0.3 for all analyses to eliminate the
material constants as parameters in the study. This assumption has an
insignificant effect on the solutions obtained, since stresses and
13
' ,p
000
00,0
0100
-4
14J
flexibilities are very insensitive to small changes in Poisson's ratio.
PRESENTATION AND DISCUSSION OF RESULTS
Finite element analyses were performed for 21 elbows with straight pipe
extensions of various lengths. The geometric data for these 21 elbows are
plotted in Figure 1. In most cases, the pipe extensions placed at each end of
the elbow were of equal length. For each of the 21 elbows, the number of
analyses performed (in order to vary the length of pipe extensions) ranged
from six to 13, the average being about 7.5. The total number of analyses
performed was 157. The stress index and flexibility factor results for all
these analyses are tabulated in detail in the Appendix.
Although our original purpose in performing these calculations was to
derive usable design equations, formulas, and curves, the complexity of the
resulting data (tabulated in the Appendix) makes this a formidable task.
This report, which is therefore a little less ambitious, will instead
summarize some of the key results indicated by the data. All observations
in this section are based on data in the Appendix.
We first consider the influence of the type of loading (moment or
force) on the results. The applied forces were chosen so as to yield the
same bending moment at the elbow middle, where stresses are generally the
greatest. The tables in the Appendix show that stress indices depend
very little on whether the applied load is a force or moment, particularly
when the pipe extensions are long. The flexibility factors are only slightly
more sensitive than the stress indices to load type for elbows with long pipe
extensions. However, flexibility factors are quite sensitive to load type for
elbows with short pipe extensions. Flexibility factors due to moment loadings
15
generally exceed those due to force loadings.
In retrospect, this independence of stress index with load type can
perhaps be explained by noting that the index depends only on the solution in
the middle of the elbow, which is always (for 90-degree elbows) sufficiently
far from the ends so as not to be significantly affected by the load type.
The elbow flexibility, in contrast, depends on the solution over the entire
length of the elbow and hence might be expected to be more sensitive than
stress index to load type.
A second question which arises is: How sensitive are stresses and
flexibilities to the length of pipe extensions? A related question is: How
long do the pipe extensions have to be in order for elbow stresses and
flexibilities to be independent of further changes in length? In Figure
4 the dependence of stress index on length of straight pipe extension (equal
at both ends) is plotted for various elbows. Figure 4 indicates that stress
indices are very sensitive to length of pipe extension for small X and
insensitive for large X. It appears that the transition from sensitivity to
insensitivity occurs near X - 0.35. Figure 4 also indicates that the critical
length of straight pipe extensions, based on stress indices, is about three
pipe diameters for X < 0.35 and one pipe diameter for X > 0.35.
Table 3 summarizes the stress index results for the 21 elbows with equal
length pipe extensions three diameters long. The actual stress indices, which
are generally greatest with long (rather than short) pipe extensions, are
grossly over-predicted in general by the idealized program ELBOW. For
internal pressure loading, the classical relation, Equation (14), is
excellent.
Flexibility factors for moment loadings exhibit a sensitivity to length
16
47% (N 0
LA; C4 u; CA 0 7
-~ ,-4 .- l .-4 en * C (O C
It U II I H H lcl
a a a a a a a a aw
CA % CA O -4 CA AOO0
44 0
C4 0 Ic.o oU
.f4
0
0 )0)
am ..-4
V4
"0
0 0
41.
14
0 N
0~~ 0%cco *
*1*4l ss l
170
TABLE 3 - STRESS INDICES FOR ELBOWS HAVING EQUAL LENGTH STRAIGHTPIPE EXTENSIONS OF LENGTH THREE DIAMETERS
NASTRAN Internal PressureELBOW
Moment Force NASTRAN Kellogg
1 .063 1.50 10.2 10.0 14.5 1.93 2.002 .126 1.50 6.55 6.41 9.28 1.89 2.003 .126 3.00 7.13 6.96 8.56 1.23 1.254 .204 1.50 4.61 4.52 6.82 1.82 2.005 .204 4.88 5.39 5.21 5.98 1.12 1.136 .210 5.00 5.31 5.18 5.87 1.12 1.137 .283 1.50 3.62 3.68 5.53 1.77 2.008 .283 6.75 4.39 4.26 4.70 1.08 1.099 .335 8.00 3.90 3.81 4.14 1.07 1.07
10 .346 1.50 3.39 3.45 4.88 1.74 2.0011 .451 10.8 3.10 3.02 3.29 1.04 1.0512 .451 1.80 2.77 2.83 3.94 1.56 1.6313 .600 3.00 2.43 2.32 2.93 1.25 1.2514 .700 3.Ou 2.12 2.04 2.61 1.25 1.2515 .973 10.2 1.67 1.71 2.00 1.05 1.0516 .975 3.00 1.76 1.80 2.13 1.26 1.2517 1.50 9.49 1.47 1.45 1.71 1.06 1.0618 1.50 3.90 1.119 1.54 1.75 1.19 1.1719 2.39 8.00 1.27 1.25 1.52 1.07 1.0720 2.39 5.15 1.32 1.37 1.52 1.14 1.1221 3.01 5.75 1.28 1.33 1.45 1.12 1.11
18
of straight pipe extension similar to that of the stress indices, except that
the transition from sensitivity (small X) to insensitivity (large X) occurs at
about X - 1.0. For flexibility factors calculated from force loadings, there
is no clear region of insensitivity. Two plots illustrating this sensitivity
are shown in Figures 5 and 6. These two figures indicate that elbows become
stiffer as the pipe extensions shorten, probably because the flanges inhibit
ovalization of the cross section.
Table 4 summarizes the flexibility factor results for the 21 elbows with
equal length pipe extensions three diameters long. There is considerable
variation between inplane and out-of-plane flexibility factors, neither of
which are predicted very well in general by the idealized approach used in the
ELBOW program; it does not distinguish between inplane and out-of-plane
moments in calculating the flexibility factor. The data listed in Table 4 are
also shown graphically in Figure 7.
CONCLUSIONS
The following conclusions apply to 90-degree piping elbows with straight
pipe extensions terminated by rigid flanges.
Stress indices are generally insensitive to whether the applied load is
a force or a staticaily equivalent moment. For elbows with long pipe
extensions at each end, flexibility factors are only slightly more sensitive
than the stress indices to load type. However, flexibility factors are quite
sensitive to load type when the pipe extensions are short. Flexibility
factors for moment loadings generally exceed those for force loadings.
Stress indices are very sensitive to length of pipe extension for
A < 0.35, where A is the bend characteristic parameter, and generally
19
00
0-
-4
'00
0
-
C1,
0
1-4 a
00 U
0)4-1
CC0)
0
C%4i
p C4 C
Lf)0 01 -
-44-
20)
-4 OD Cn 4fc~C-4 C 'C4 CVn -T0
0
4 -41
0)
w- 44
P4 )
0
-'4
0
00
.
0
0N.
- 4
U,)
C14 0
-44
Lf) C" CLei 0" C
A2 T44xa4
210
TABLE 4 - FLEXIBILITY FACTORS FOR ELBOWS HAVING EQUAL LENGTH STRAIGHT
PIPE EXTENSIONS OF LENGTH THREE DIAMETERS
NASTRAN (Moment) NASTRAN (Force)y ELBOW ASME
Inplane Out-of-Plane Inplane Out-of-Plane Code
1 .063 1.50 21.8 9.84 20.9 10.1 27.5 27.5
2 .126 1.50 11.3 5.44 10.8 5.47 13.8 13.7
3 .126 3.00 11.3 5.86 10.7 5.85 13.8 13.7
4 .204 1.50 6.98 3.62 6.63 3.58 8.49 8.48
5 .204 4.88 7.18 4.09 6.63 3.94 8.49 8.48
6 .210 5.00 7.03 4.02 6.54 3.91 8.27 8.24
7 .283 1.50 5.04 2.79 4.76 2.71 6.09 6.11
8 .283 6.75 5.28 3.23 4.80 3.04 6.09 6.11
9 .335 8.00 4.47 2.85 4.05 2.67 5.09 5.16
10 .346 1.50 4.14 2.41 3.89 2.31 4.92 5.00
11 .451 10.8 3.32 2.31 2.95 2.09 3.69 3.84
12 .451 1.80 3.19 2.05 2.91 1.92 3.69 3.84
13 .600 3.00 2.48 1.82 2.27 1.70 2.71 2.88
14 .700 3.00 2.15 1.67 1.97 1.55 2.32 2.47
15 .973 10.2 1.65 1.48 1.47 1.33 1.73 1.78
16 .975 3.00 1.69 1.46 1.59 1.37 1.73 1.77
17 1.50 9.49 1.30 1.31 1.15 1.16 1.32 1.15
18 1.50 3.90 1.35 1.31 1.23 1.20 1.32 1.15
19 2.39 8.00 1.14 1.23 1.02 1.10 1.13 1.00
20 2.39 5.15 1.17 1.24 1.07 1.13 1.13 1.00
21 3.01 5.75 1.14 1.23 1.00 1.08 1.08 1.00
22
1-4 0
0 ) 0 ro
r4 4..
~ 0 ;j
1-4 0 -w
0 w 0
o -4 .~.
V P4
0 0
4- w0.~
.- 4 W
44.
"4 00
00 -4 4
0% (a
-12341AIT4TX~
239
insensitive for X > 0.35. The critical length of straight pipe extension
(defined as the minimum length of pipe for which the stress index is
insensitive to further increases in pipe length) is about one pipe diameter
for X < 0.35 and three diameters for X > 0.35.
For elbows loaded by internal pressure only, the stress indices are
insensitive to the length of straight pipe extension. The theoretical
predictions by the classical relation given in the Kellogg book for this case
are excellent.
Flexibility factors exhibit a sensitivity to length of straight pipe
extension over the entire range of elbow parameters considered. Flexibility
factors for out-of-plane loading differ considerably from those for inplane
loading.
The fast-running computer program ELBOW, which idealizes elbows as
sections of tori, is generally not adequate for predicting stress indices or
flexibility factors for 90-degree elbows with straight pipe extensions.
RECOMMENDATIONS
Although a large quantity of useful data has been compiled in this
report, the report is viewed as interim, since the information is not in a
form to be easily used by a piping system designer. We therefore recommend
that the data presented here be analyzed fuither to obtain usable design
equations, formulas, or curves for 90-degree elbows with straight pipe
extensions.
Since not all elbows used in naval designs are 90-degree elbows, we
recommend that other bend angles (e.g., 45 degrees) be investigated. Also,
future parametric studies would be less expensive if a more restrictive
24
selection of elbows is made.
The presence of an internal pressure preload is known to have a
significant effect on momen; stress indices and flexibility factors. A finite
element procedure for this combined loading case, which is mathematically
nonlinear, needs to be formulated and validated. Following such validation,
the various parametric studies discussed above (for which the internal
pressure is zero) should be repeated for several typical nonzero pressure
levels.
ACKNOWLEDGMENTS
We acknowledge with pleasure the fruitful discussions held with Mr.
L.M. Kaldor and Dr. Y.P. Lu of the Machinery Silencing Division (Code 274).
25
APPENDIX
Tables of Finite Element Results for 90-DegreeElbows with Straight Pipe Extensions
27
C- -4
r4 U 4.w0. 0 00 N
40)
0-
0P 00 V Ln M~Q
. - O4C14
- 1-4
3 - -L f f
1J -4 0%MM0C40w
04 ON 14-4 o*L 4 44a:r
-' 0
E- -1 W
m~ 0 _:8C ;L 0 r.. C91 1 NC1 11 -4 )41 4
4 >%CJ~
144
-4 V)
Ci) 41 -- 4 V4
W W) ;K,0 b
C14~~~1 0 nCDI "
rar.4 co -4
E-4~~~0 41w nN )%4o M00 40 nM-: 7 c.,cn D
w~ 0 C)0C0 zAC4C
0
14Lf4 c.
-4 14 -r -- - -- 4- -
29
.$4 0 Ln LA 4
0 -
en U-) 0 C'-4
ci 4 . .0. 0 0 1: ;C4-
14
3-0
41J -4 00
.0 ) 0 Ln UP) - C' C'4
7, -40 IAO 4) - 0 01
cc o C) .)C d)(n:4 r-
E-4 -4 0 : 4L4!4 c 44 4
za 0 - x , -1
"-4 V
(7 c 00 %Dr- C
w N~$ 0) 04 ) (A2U2 J .I -4 a)
C) 11r-~-N C)b
LO4 CO r 0~ 0w~ $4 00 4 M-1 14 :C12 0 4 =z-
z
t: C:w ( 0C
0
4: C
Lf4
014-H 4 ~C14 CN C
30
-4 ) '-
40
4) -
0-z 4
V)J -4
- 4-4
00 Q)
04 0I
Ca f4
1-.4 1. *
.4) 0 cr f r ~ V)e 1 n mC 4S
x '- A0
E-44
1- Ai u C ~~~j4
1-4 ~~~~~ ~ ~ ' Cu W4 1 NC -4 wC14 - 14 4)W
4) 4) N o L N m mL -b
41 $4 0 W -U) 0 L.41 pq ZA * -
E'4 41 D( C,-4 -4 - -- 4 -4 4 00 .0 .-I (
oA 4- C4 z) z4-i4
CA . .- .-. .00 i2CD 10 %0
4- .. 90 00 0 0.4 4.-42 1-4 M-.2I 0)e nrn ne e nme
I3
1-4
-4 l
0-1
Z Aj
1-4
0
Q)
4J .-4 CN CY 00 0
0. C0 O ll re1 0J0 C
.0 Q.) 0 CYICnM ' MC14 C'J
-4*4 0
z0 04.
F-4 to -4 %0 N0 sC4-t-1 - Ycn~' ;L 4Wwcu p
U -AJ - Q
3 -4P- u >
E.W ww ww w m r-4 x
r& a) U) . . .- . . . . .
O1 0) 4-
Ui) 4 -4U) C) 0 bio
Lm w l Ln 42 lbC L 1
4-' 0. 00 14 1;1 4114c c -4
w LU
V) % % i M CN M LfDC4 CD
0
.0If4 -T
32
*1- CCj rI.4C'4 1.4 0 ~cv'JC) qNJ
04$44
U a)
'-4 * oC sC40
LfI
%a 4)
414 -4 N0 m
-, 0 4-4
E- 0) 0 AjC'~J '
z 0 0
E-441 Q) 0 w4) r. O Cr- A'." (.)
00 -4 Cd 1 Nr oO QQ 4
4 A-. 0
Zu
0)z 4) X4-4 V-
z 0 C4 !CJ0 C4 C-4 CN )-H- -H
4) 3-. . . . . A ) 0CN W .0 4)
144) x3 4.e'0.t1-4 4) Q)U(N ~ 0j4 4. La4 bo0-
w, Q) - , 140
$4C40)0 C4C t3
;4
000
33)
0
-44
,- 4 U V 4-4 n 0% a
04
o to
4) 0 -4 1
o- x 0 O1 11 11 .
$4 4.
0~~~~~ GJ C -- t'cC'CJ'
r- mJ 1. w m r1 4liii
E-4'- 0 cor O iMLnu
0 z . -1 o $
E- C0 0 00%O6L~ ~
'-a 4-1 X
x 1-4 VE-4 0) >,-M- r_
-4 5.4V
z C :jS. *4 4r
x 4)4x U
S.. U . 0 *'0 4 Q 0Vi (U .0 ~ -4
0i C... AA) l)
C.. a) M 7 00U
z t
I.-. -- -r r '
V)~ C'J
00
.- 4w
34
0 1
4.
0
u 41
00
-H . 0O a%. 00 C)V)ON00 )
I- 4-4 . . . .L
0)4
CAO
z 0 :20
E-4 C 0N .$ II 0 4-I 0
tn EL0) C114 - 4 C4C C P L
E-4~~ ~ r- ~41 4o
zZ -O o r0~t- 4 cl)
1- -C4 0)1.41 1
0 wa) ~~ ~ 0. 4) 00 C1 T :r
w Q uor-Ln.. r
w- 0 W -
En4 0 c4 9c 4c )X -4)Ene 0) 0)i
%0 C11 Co,4Z 1.
0)~Lf 0)c-c l-.
CjC4
0
35
-4 1 J ON 0-- C'JCC-4 %64 . . . . ..0 $ 0 en C4 "C-4CJ.,1 0 1
0
md -4 - Y M C
z c-
0
on Q)I
.4 r4~ .
-4- 0- N O
1 C1 000U) e
C 1 4 cu4. .. . U. .0) 0 '- C4C4 1 -
x~~ 0 4J 11I
w I"~-4~A 0 ) 00 00 (A~4~4
MJ 4 X
03 00 '-0 0000000 - -
Q) 4
0 wJ
"o V)C , ,U bw u C14 00 %0 40
41 w 0 0 w -
0
.0L )LnC4
ll 36
1v4
Ci 4. * *
0
00
0 44 . . . . . 1; U
0% 0
Aj 0%.C -0 o- Ii r. r -* 1VrL. r - 4) 6
00W 0 >4'JCe4
oC-E O
;I cc. -.. 00Z 0 4 ~O -4 4)
1-4
0) - 1 T0 v rU w
0) ~ 00 env- m O)(nwn
E-4 41 0 m0O 00
0)r
Z05 'JC
.0~~- ,-4 onUQ Lr-I~Ci. 0h CY % N
a) d e'J~~Oc-~37
-D W 4 0
0
- ~ ~ ~ ~ L .. 0 W'C C'- C'J'-1 W~0 I
Ca.4 m m C4
z 1.
00
"4 P. 00 m 0 0
LA Cu
to-4 is 4 I C 0
Z o'$4 0
0 tC-. E-4 cd c
&' Cu4 Cu1 -4- 0 -- ? % '-u ca)
4. -H W
W cu ol.
$4 C/)
414) 0)mm C Y nC)c nc 4 C
-4 %0 5I *0 %0 .fQ -
w-' 0)) U)4 *w- C,4
0) - - - - -U). 40C . ) -4 .
o a 0)38
0
41
-4 04 Inr0 1N 0 N -- -
r-40
N~2 C1 N C
E-4 X 0.
0
g~ " w - 0
w C 0
o~~t Aj X)-0 0 -0
(A 0000000 0 0 C'N N NN N CIU, .,--4 vE-44- X O. I- I I II
0-4 Ow 0 -1U) cn
9-4 1.
u -- HO 0 0
w -04-LO~~~* 0 JJ C4C o oz
(n---- - -3. -4
H 0 0 4.- 4 C
E-4 1. V J
-4~~1 '-4 ) Cl) 00 0 00 0 0 4
LAf 0 )-. 7 ~ ~ ~ Lf Ln0- - - - - - -0 0
~~Z4~C (14 U .4 ~ 9
o ~0. J
L owalAC~. 0 1.m0 -----
PL. Wf - nr
z
cc 0% 0% %0 Ln
t-4
4)
A- -4 -rO tC
0)
-4£~~-r~
41 ) 0 w'~4~~-
v C1MM-1 14- 4 -o
.4 -4
X Cf ~ tLf~L~%O O t44 - W
* ~ 1-4W4(. t-4
It- 04 4_ 4 :1 0
4) 4)
w 0 0 wto 0 4141 4 ;1
04
0)
c1 C4 0 4.4
z4
40) _ _ _cn q a Io
w
00 a)w
4 L 4C41 1: 4.4 0 44 OwCJzd _0 -4>,1
U, 0)
~-.4 q)s
0 - .04 (v x 4-
>4 -4- -4 0 1
w- "a 00)
44 0 4 C4 4 4 14 14 ; ca- 4 l
E-4 AC M) Cl) M *4a 4) -4 (n)0~ C
0 C-4 C).i G)X c-4 c
64 $.4 N) W
Al rne nen()e
.0.) ~ ~ ~ ~ -4 * * * * 0
0-41
-,4 04'- n-* 0 0 1
1-4 1 I f n t*-4 (J 4~4.0 w- 0 - - - -
,0 1-
-4Cfl C '=4-_
00u )
< -4
.fH PL) 0 , Ln CY -i -4 C'4
Hx H 44 .O C-4 11 14
Q) 0Ln s I
E- 0I~ A4* Ci.
* z 040'
g " 4 - 0~ (aiu . )V - 00 Ln Za
C)O 4 4C 4 P.-
E-4 0r r. CC C-eJ'CJ'J' -1 4
r-4 Ai CI C O -4
o- C4 04 C4C 4C1 - X CA'4. C)O Q) W . . . . . ." ) M~
10 -) 1 A 44
U) w~L 0 bo
ci 0 %)y C) 0~C' 3: :9
1. 0 00 -4
Q C 4~ C) 4 00'00
z IS C1 cN C14 '-4C'-J
L/n C14J
. 1; . .4
0-4 0-4 -- - -
42
-14r-.,4,- 0. M 0 D4n--4 0) I JC'.C"JC'"-4 U 4
.0 S. 0 -- - -
H 0
E4 rx .m -IT -- n04V
41 -4 0 ( oL
... 4.-0 04 r- Or-r-T
-- , C4:w 4-.-'-0
-4 CC4
4 0. 00D %- nLnL
1-'i >% W .40
H- XC 0000001-94 . . .* . . *.0C~~- Ci -- 4 - .0 -4C
'-4 ok wiCA 414
>4 r-4 "0 b
mi Ci 00f i Lbo
'A 0- 0J0CJ
0z 00g -
'-34
'A
-4 -4 1 e----
43
41 -4
$4 04 ~ .fJ ~ O L- 0 I
x 4 4-4
-4C
o "
Cd - - -4T
-44 -4
0-
-4 -IT-IT'T 4
- '44 . . . . . . . 4 - 44l -4) 0 -
.- '- 09 4 4 0 c
1-4 - M r - d(m m o I' 1.0 o oLM L
04- r .- ow
45. u >N
-4.10. -4 N . .. N 04- XC
-H W0
(a4 Ci) *4 *- 0 )
4. -4 W0-0
W U) FL0 0 Cl)0) ,-< 0% 0 .-4 T 0
p ~ ~ ~ ~ ~ ~ / u Cl 00bi) ) e3
5.. 0 w~~0 3:3 1
%0 ID %Q 00'4CDL
'00
CnC*
0 0
44
4-4 4000%0L04 '- 0 C)
..-4 u 4-4 . . . . . .
.0 w~ 0 - - -
.- 0 1
r14 w ..
000
E-4~ 044 C 440000 ~ c-
0~- C44 4.M I ..
~5q v4 C: 44 *- -O.0 0) 0
041 00
C. 4 $4 c00 0'
i1to 41 X.8 O.
1-4 0 W 0000 0--X
*~( ~ 4.0 - 40 4) OX 4.
w) -)4
Lra Uj -4.'7.7 . - 0W1. 1.4 8 00 O
4 . w 0 W * *-4-4-4-4--=4-
E-4i
L~Ln
S4
-4-. -- 4 -4 -4 -4
45
.,C.) ~ r-..%0 C4 0
-4 U 4-. . . .00 w 0
r4 0 I
-4
0 -
Z 41
4 .c ---- 0-4
00
.-4 -, - ., 0 CON P- en - -;o -, CC:C44 .)C. . . . .
W.0 4 0 -4---4 .
z 0i
0 - o 5.en4 c n naN~~ ~ U)4rW t
0 0. -4--4
Zd 4.1'-r4
x .- 4
-4 "a 0 - 4 4.0
C:~ w W44 - - -H 444 0 w *.-41>4 4 0) Wi -4 4 4 4 4)..4
W~ En boWi ci wl V) C'J o0 (.) bO1.) 0 00z-
.. 4 cnz
0
in
Li,
-4 1-4 -4 4 - 4
46
64 00
.*0
C-'4 0l 0%)O %O
C-4 14C4 S0a -- 4
0
cn 00z
Cr21 0 -- --cc4 m -4Q Q
ow.4 0 44
1. -.
to oww Ps0 0z 414 00 -
ONx 00 ) ) 0 r1.40
-4 .-0 -4 w4
0- .0 0
44 -.4 - 4
w 14 04 0 0 0 0 00N-4-t 3: 041 kA . '00 00 -
-4 4 P4 V) 4
C14 - 1 C___ _ __4 _ _ 1.4 01 0 C
P-3z 00b
-L Cr4
14 00 W44'
474
0 V
0
4j
m4 0 044h O
4-..)
L1'- .
0i0
F4u- CO~ (a O
zr COr3 . . . . . .M
"14 -4- -- 0P4A
ri - a
0-44
'-4 x co 1-4 X M
0)-0 14 Q
00 4) 0 A---
xo~~ ~ c 4- l ) l
'1hz mCO 1C-4
144 LIC'
cq sOC -4
.00 0 00 0 0044 N 4N 14 C4
48
4 en 4.4(
wO~ 0
4)0 -
u 4) C14 - - n -I n
ca C: 0 % n00 -
44 ,.0. %0 0 % %a
C14 0 0 .3-4 4
onJ
1.4 Ai r4i 0
0~~~~. 4.1 41 1 C4C1 4iJ 1-A- 0 04 . . . . . . .a
0) -. 1- -414 -4 0L..
oU Ai ~
F4 0c X4 -49: ua)
zz
-4 x 'C'~jC4~4'
-4CA - -44 -- -4 -41 X -4r 0 0 I *q 0 to
0) CU -4 V).0 -4 w
W ~ ~ C - A - L0 - 04 b
Go WJ ;1 0
G)~ 4.1 m. *1 0 0 -00r -L
w .* 0fj0.Ii-4
.gn 0 -4 co -4- --4-4 c' 4C)Nc)
L49
4. 00 0 00 00En~~~~~~~' C: C4C C4C4C1 1
REFERENCES
1. Marcus, M.S., and G.C. Everstine, "Finite Element Analysis of PipeElbows," Report CMLD-79/15, David W. Taylor Naval Ship Research andDevelopment Center, Bethesda, Maryland (Feb 1980).
2. Quezon, A.J., G.C. Everstine, and M.E. Golden, "Finite ElementAnalysis of Piping Tees," Report CMLD-80/11, David W. Taylor Naval ShipResearch and Development Center, Bethesda, Maryland (June 1980).
3. Quezon, A.J., and G.C. Everstine, "Comparison of Finite ElementAnalyses of a Piping Tee Using NASTRAN and CORTES/SA," Ninth NASTRAN Users'Colloquium, NASA CP-2151, Washington, D.C., pp. 224-242 (Oct 1980).
4. Dodge, W.G., and S.E. Moore, "Stress Indices and Flexibility Factorsfor Moment Loadings on Elbows and Curved Pipe," Report ORNL-TM-3658, Oak RidgeNational Laboratory, Oak Ridge, Tennessee (March 1972).
5. The M.W. Kellogg Company, Design of Piping Systems, Second Edition,John Wiley and Sons, Inc., New York (1964).
6. Dodge, W.G., and S.E. Moore, "ELBOW: A Fortran Program for theCalculation of Stresses, Stress Indices, and Flexibility Factors for Elbowsand Curved Pipe," Report ORNL-TM-4098, Oak Ridge National Laboratory, OakRidge, Tennessee (Apr 1973).
7. American Society of Mechanical Engineers, "ASME Boiler and PressureVessel Code. Section III, Rules for Construction of Nuclear Power PlantComponents" (1980 edition).
51
4.!
INITIAL DISTRIBUTION
Copies
13 NAVSEA1 SEA 05D3 SEA 05D121 SEA 05R2 SEA 05R142 SEA 5322 SEA 5332 SEA 996122 SEA 09G32/Lib
12 DTIC
1 Oak Ridge National Laboratory(Union Carbide Nuclear Div.)
1 S.E. Moore
1 Combustion Engineering, Inc.
Chattanooga, TN >
CENTER DISTRIBUTION
Copies Code Name
1 18 G.H. Gleissner2 1509.3 D. Harris1 184 J.W. Schot1 1844 S.K. Dhir4 1844 G.C. Everstine4 1844 A.J. Quezon1 27 W. Dietz1 274 L. Argiro1 2740 Y.F. Wang1 2744 D. Allvein5 2744 L. Kaldor1 522.1 Unclassified Lib (C)1 522.2 Unclassified Lib (A)
53
DTNSRDC ISSUES THREE TYPES OF REPORTS
1. DTNSRDC REPORTS, A FORMAL SERIES, CONTAIN INFORMATION OF PERMANENT TECH-NICAL VALUE. THEY CARRY A CONSECUTIVE NUMERICAL IDENTIFICATION REGARDLESS OFTHEIR CLASSIFICATION OR THE ORIGINATING DEPARTMENT.
2. DEPARTMENTAL REPORTS, A SEMIFORMAL SERIES, CONTAIN INFORMATION OF A PRELIM-INARY, TEMPORARY, OR PROPRIETARY NATURE OR OF LIMITED INTEREST OR SIGNIFICANCE.THEY CARRY A DEPARTMENTAL ALPHANUMER;CAL IDENTIFICATION.
3. TECHNIC;AL MEMUHANDA, AN INFORMAL SERIES, CONTAIN TECHNICAL DOCUMENTATIONOF LIMITED USE AND INTEREST. THEY ARE PRIMARILY WORKING PAPERS INTENDED FOR INTERNAL USE. THEY CARRY AN IDENTIFYING NUMBER WHICH INDICATES THEIR TYPE AND THENUMERICAL CODE OF THE ORIGINATING DEPARTMENT. ANY DISTRIBUTION OUTSIOE DTNSRDCMUST BE APPROVED BY THE HEAD OF THE ORIGINATING DEPARTMENT ON A CASE-BY-CASEBASIS.
I...." ........................... ............. I : I' ::::' -I i. .. ;n