CAESAR II Quick Reference Guide

Version 5.10 CAESAR II Quick Reference Guide

Copyright © 1985-2008 COADE, Inc. All Rights Reserved.

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Quick Reference Guide Version 5.10

1

CAESAR II Quick Reference Guide Version 5.10 The CAESAR II Quick Reference Guide is intended to aid users in quickly identifying needed information and to resolve common questions and problems. This Reference Guide is distributed with each copy of the software and users are urged to copy the Reference Guide as necessary. Comments and suggestions concerning CAESAR II, the User Guide, or the Quick Reference Guide are always welcome. Users with problems, questions, or suggestions can contact the COADE Development/Support staff at: [email protected].

CAESAR II Quick Reference Guide Table of Contents CAESAR II Quick Reference Guide Version 5.10.......................................................................1 CAESAR II Software ..............................................................................................2 CAESAR II Pipe Stress Seminars ...........................................................................2 System Requirements ..............................................................................................3 Troubleshooting.......................................................................................................3 CAESAR II Interfaces .............................................................................................3 Piping Codes............................................................................................................4 Restraints .................................................................................................................5 Setup File Directives List ........................................................................................6 List of Materials.....................................................................................................11 CAESAR II Intersection Types .............................................................................12 Code Stresses .........................................................................................................13 Node Locations on Bends......................................................................................24 CAESAR II Quality Assurance Manual ................................................................26 Mechanical Engineering News ..............................................................................26 Additional COADE Software Programs................................................................26


2


CAESAR II Software CAESAR II is an advanced PC based tool for the engineer who designs or analyzes piping systems. CAESAR II uses input spreadsheets, on-line help, graphics, and

extensive error detection procedures to facilitate timely operation and solution. CAESAR II is capable of analyzing large piping models, structural steel models, or combined models, both statically and dynamically. ASME, B31, WRC, and rotating equipment reports combine to provide the analyst with a complete description of the piping system’s behavior under the applied loading conditions. Additional technical capabilities such as out-of-core solvers, force spectrum analysis (for water hammer and relief valve solutions), time history, and large rotation rod hangers provide the pipe stress engineer with the most advanced computer based piping program available today. CAESAR II is continuously enhanced to incorporate new technical abilities, to provide additional functionality, and to modify existing computation procedures as the piping codes are updated. A complete list of the most recent changes to CAESAR II can be found in the Chapter 1 of the User Guide. Users wanting software sales are urged to contact the COADE Sales staff at: Phone:281-890-4566

E-mail: [email protected]

FAX: 281-890-3301

Web: http://www.coade.com/product_overview.asp?varflag=CAESARII

CAESAR II Pipe Stress Seminars COADE offers seminars periodically to augment the Engineers knowledge of CAESAR II and Pipe Stress Analysis. The general seminar is held in our Houston

office and covers five days of Statics. Twice yearly we also cover five days of Statics and three days of Dynamics. These seminars emphasize the piping codes, static analysis, dynamic analysis, and problem solving. Custom seminars held at client locations are also available. For additional seminar details, please contact the COADE Support staff at: seminars @coade.com.



3

System Requirements CAESAR II requires Windows 2000, or Windows XP Professional, with a

minimum graphic card capability of 1024x768 resolution. However, for more efficient usage of the software, higher graphics resolutions are necessary. Usually any hardware capable of running these operating systems will be sufficient to run CAESAR II. For effective use of CAESAR II, COADE recommends as a minimum configuration: 2+ Ghz processor 1+ Gbytes of RAM 1280x1024 graphics resolution or better 256+ Mbytes of video RAM Windows 2000 or Windows XP Professional Please note that Windows XP Home Edition, Windows Vista Professional and Windows Vista Home Edition are not supported.

Troubleshooting For troubleshooting and problem solving issues, refer to the CAESAR II Frequently Asked Questions (FAQ) located on the COADE Website. To access the FAQ: (http://www.coade.com/product_faq.asp?varflag=CAESARII&varflagmaster=). CAESAR II Interfaces There are several external interfaces which allow data transfer between CAESAR II and other software packages. Users can access these interfaces via the Tools menu on the CAESAR II Main Menu. CADWorx

requires AUTOCAD

AUTOCAD

DXF Output

COMPUTER VISION

mainframe

INTERGRAPH

mainframe

CADPIPE

requires AUTOCAD

ISOMET

mainframe

PDMS

mainframe

PCF

Alias format

Users interested in these interfaces should contact COADE for further information. We anticipate other interfaces in the future keep users updated via the newsletter or revised documentation.


4


Piping Codes The table below displays the Piping Code, publication and/or revision date. PIPING CODE

PUBLICATION

REVISION

ANSI B31.1

(2004)

December 15, 2006

ANSI B31.3

(2006)

May 31, 2007

ANSI B31.4

(2006)

October 20, 2006

ANSI B31.4 Chapter IX

(2006)

October 20, 2006

ANSI B31.5

(2001)

May 30, 2005

ANSI B31.8

(2003)

February 6, 2004

ANSI B31.8 Chapter VIII

(2003)

February 6, 2004

ANSI B31.11

(2002)

May 30, 2003

ASME SECT III CLASS 2

(2004)

July 1, 2005

ASME SECT III CLASS 3

(2004)

July 1, 2005

U.S. NAVY 505

(1984)

N/A

CANADIAN Z662

(6/2003)

N/A

CANADIAN Z662 Ch 11

(6/2003)

N/A

BS 806

1993, ISSUE 1, SEPTEMBER 1993

N/A

SWEDISH METHOD 1

2ND EDITION STOCKHOLM 1979

N/A

SWEDISH METHOD 2

2ND EDITION STOCKHOLM 1979

N/A

ANSI B31.1

(1967)

N/A

STOOMWEZEN

(1989)

N/A

RCC-M C

(1988)

N/A

RCC-M D

(1988)

N/A

CODETI

(2001)

June 2004

NORWEGIAN

(1999)

N/A

FDBR

(1995)

N/A

BS7159

(1989)

N/A

UKOOA

(1994)

N/A

IGE/TD/12

(2003)

N/A

DnV

(1996)

N/A

EN-13480

(12/2006)

Issue 9

GPTC/192

(1998)

N/A

PD 8010 Part 1&2

(2004)

N/A



5

Restraints No.

Restraint Type

Abbreviation

1

Anchor

A

2

Translational Double Acting

X,Y, or Z

3

Rotational Double Acting

RX, RY, or RZ

4

Guide, Double Acting

GUI

5

Double Acting Limit Stop

LIM

6

Translational Double Acting Snubber

XSNB, YSNB, ZSNB

7

Translational Directional

+X, -X, +Y, -Y, +Z, -Z

8

Rotational Directional

+RX, -RX, +RY, etc.

9

Directional Limit Stop

+LIM, -LIM

10

Large Rotation Rod

XROD, YROD, ZROD

11

Translational Double Acting Bilinear

X2, Y2, Z2

12

Rotational Double Acting Bilinear

RX2, RY2, RZ2

13

Translational Directional Bilinear

-X2, +Y2, -Y2, etc.

14

Rotational Double Acting Bilinear

-RX2, +RY2, - RY2, etc.

15

Bottom Out Spring

XSPR, YSPR, ZSPR

16

Directional Snubber

+XSNB, -XSNB, +YSNB, etc.


6


Setup File Directives List The following list represents the possible directives which can be controlled by the user via the CAESAR II configuration file CAESAR.CFG. These directives can be changed by the user through the use of the CONFIGURE-SETUP program, accessed via Main Menu option #9. Directives are listed in groups corresponding to the configuration program's menu options. Geometry Directives GEOMETRY DIRECTIVES

CONNECT GEOMETRY THRU CNODES =

YES

34

MIN ALLOWED BEND ANGLE =

.5000000E+01

36

MAX ALLOWED BEND ANGLE =

.9500000E+02

37

BEND LENGTH ATTACHMENT PERCENT =

.1000000E+01

38

MIN ANGLE TO ADJACENT BEND PT =

.5000000E+01

39

LOOP CLOSURE TOLERANCE =

.1000000E+01

42

THERMAL BOWING HORIZONTAL TOLERANCE =

.1000000E-03

92

AUTO NODE NUMBER INCREMENT=

1000000E+02

109

Z AXIS UP

NO

129

USE PRESSURE STIFFENING =

DEFAULT

65

ALPHA TOLERANCE =

.5000000E-01

33

HANGER DEFAULT RESTRAINT STIFFNESS =

.1000000E+13

49

DECOMPOSITION SINGULARITY TOLERANCE =

.1000000E+11

50

BEND AXIAL SHAPE =

YES

51

FRICTION STIFFNESS =

.1000000E+07

45

FRICTION NORMAL FORCE VARIATION =

.1500000E+00

47

FRICTION ANGLE VARIATION =

.1500000E+02

48

FRICTION SLIDE MULTIPLIER =

.1000000E+01

46

ROD TOLERANCE =

.1000000E+01

59

ROD INCREMENT =

2000000E+01

58

Computation Control COMPUTATION CONTROL



7

COMPUTATION CONTROL

INCORE NUMERICAL CHECK =

NO

60

DEFAULT TRANSLATIONAL RESTRAINT STIFFNESS .1000000E+13

98

DEFAULT ROTATIONAL RESTRAINT STIFFNESS =

.1000000E+13

99

IGNORE SPRING HANGER STIFFNESS =

NO

100

MISSING MASS ZPA =

EXTRACTED

101

MINIMUM WALL MILL TOLERANCE =

.1200000E+02

107

WRC-107 VERSION =

MAR 79 1B1/2B1 119

WRC-107 INTERPOLATION =

LAST VALUE

120

INCLUDE_INSULATION_IN_HYDROTEST=

NO

147

AMBIENT TEMPERATURE =

70.00

135

BORDER PRESSURE =

NONE

136

COEFFICIENT OF FRICTION =

0.

140

INCLUDE SPRING STIFFNESS IN FREE THERMAL CASES =

NO

141

REDUCED INTERSECTION =

B31.1 POST1980

32

USE WRC329 =

NO

62

NO REDUCED SIF FOR RFT AND WLT

NO

53

B31.1 REDUCED Z FIX =

YES

54

CLASS 1 BRANCH FLEXIBILITY

NO

55

ALL STRESS CASES CORRODED =

NO

35

ADD TORSION IN SL STRESS =

DEFAULT

66

ADD F/A IN STRESS =

DEFAULT

67

OCCASIONAL LOAD FACTOR =

.000000E+00

41

DEFAULT CODE =

B31.3

43

B31.3 SUSTAINED CASE SIF FACTOR =

100000E+01

40

ALLOW USERS BEND SIF =

NO

52

USE SCHNEIDER =

NO

63

YIELD CRITERION STRESS =

MAX 3D SHEAR 108

SIFS and Stresses SIFS AND STRESSES

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8


SIFS AND STRESSES

BASE HOOP STRESS ON =

NO

57

EN-13480 use in-plane/out-plane SIF

NO

133

LIBERAL ALLOWANCE =

YES

137

STREE STIFFENING DUE TO PRESS =

NO

138

B31.3 WELDING/CONTOUR TEE MEET B16.9 =

NO

139

IMPLEMENT _B31.3_APPENDIX_P

NO

144

IMPLEMENT_B31.3_CODECASE

NO

145

B31.3 Sec 319.2.3(c), Saxial

NO

146

PRESSURE VARIATION IN EXPANSION CASE DEFAULT =

DEFAULT

143

USE FRP SIF =

YES

110

USE FRP FLEXIBILITY =

YES

11

BS 7159 PRESSURE STIFFENING =

DESIGN STRAIN 121

FRP PROPERTY DATA FILE =

CAESAR.FRP

122

AXIAL MODULUS OF ELASTICITY

3200000E+07

113

RATIO SHEAR MOD : AXIAL MOD =

2500000E+00

114

AXIAL STRAIN : HOOP STRESS

1527272E+00

115

FRP LAMINATE TYPE =

THREE

116

FRP ALPHA =

.1200000E+02

117

FRP DENSITY =

.6000000E-01

118

EXCLUDE F2 FROM BENDING STRESS (UKOOA)

NO

134

PIPES

LIGHTCYAN

1

HIGHLIGHTS

GREEN

2

LABELS

GREEN

3

BACKGROUND

BLACK

5

FRP Properties FRP PROPERTIES

Plot Colors PLOT COLORS

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9

PLOT COLORS

HANGER/NOZZLES

BROWN

16

RIGID/BENDS

LIGHTGREEN

17

NODES YELLOW

YELLOW

18

STRUCTURE

LIGHTRED

31

DISPLACED SHAPE

BROWN

30

STRESS > LEVEL 5

RED

24

STRESS > LEVEL 4

YELLOW

25

STRESS > LEVEL 3

GREEN

26

STRESS > LEVEL 2

LIGHTCYAN

27

STRESS > LEVEL 1

BLUE

28

STRESS < LEVEL 1

DARKBLUE

29

STRESS LEVEL 5

.3000000E+05

19

STRESS LEVEL 4

.2500000E+05

20

STRESS LEVEL 3

.2000000E+05

21

STRESS LEVEL 2

.1500000E+05

22

STRESS LEVEL 1

.1000000E+05

23

STRCT DBASE =

AISC89.BIN

70

VALVE & FLANGE =

CADWORX.VHD 90

EXPANSION JT DATABASE =

PATHWAY.JHD

91

PIPING SIZE SPECIFICATION =

ANSI

88

DEFAULT SPRING HANGER TABLE =

1

112

SYSTEM DIRECTORY NAME =

SYSTEM

123

UNITS FILE NAME =

.ENGLISH.FIL

124

LOAD CASE TEMPLATE =

.LOAD.TPL

142

ENABLE ODBC OUTPUT

NO

128

APPEND RE-RUNS TO EXISTING DATA

NO

126

ODBC DATABASE NAME

127

Database Definitions DATABASE DEFINITIONS


10


Miscellaneous Computations MISCELLANEOUS COMPUTATIONS

OUTPUT REPORTS BY LOAD CASE

YES

87

DISPLACEMENT NODAL SORTING

YES

89

DYNAMIC INPUT EXAMPLE TEXT

MAX

94

TIME HIST ANIMATE

YES

104

OUTPUT TABLE OF CONTENTS

ON

105

INPUT FUNCTION KEYS DISPLAYED

YES

106

MEMORY ALLOCATED

12

NA

USER ID " "

NA

DISABLE _UNDO

NO


128


11

List of Materials The CAESAR II Material Table contains 17 different isotropic materials. Properties and allowed temperature ranges for each isotropic material are listed below. Material No.

Material Name

Elastic Modulus

Poisson's Ratio

Pipe Density (lb./cu.in)

Temperature Range (deg. F)

1

Low Carbon Steel

29.5 E6

0.292

0.28993

-325

1400

2

High Carbon Steel

29.3 E6

0.289

0.28009

-325

1400

3

Carbon Moly Steel

29.2 E6

0.289

0.28935

-325

1400

4

Low Chrome Moly Steel 29.7 E6

0.289

0.28935

-325

1400

5

Med Chrome Moly Steel 30.9 E6

0.289

0.28935

-325

1400

6

Austenitic Stainless

28.3 E6

0.292

0.28930

-325

1400

7

Straight Chromium

29.2 E6

0.305

0.28010

-325

1400

8

Type 310 Stainless

28. 3 E6

0.305

0.28990

-325

1400

9

Wrought Iron

29.5 E6

0.300

0.28070

-325

1400

10

Grey Cast Iron

13.4 E6

0.211

0.25580

70

1000

11

Monel 67% Ni/30% Cu 26.0 E6

0.315

0.31870

-325

1400

12

K-Monel

26.0 E6

0.315

0.30610

-325

1400

13

Copper Nickel

22.0 E6

0.330

0.33850

-325

1400

14

Aluminum

10.2 E6

0.330

0.10130

-325

600

15

Copper 99.8% Cu

16.0 E6

0.355

0.32270

70

400

16

Commercial Brass

17.0 E6

0.331

0.30610

-325

1200

17

Leaded Tin Bronze 1

14.0 E6

0.330

0.31890

-325

1200

In addition CAESAR II supports material types 18 or 19 for cut short and cut long cold spring elements. Material number 20 activates the CAESAR II Orthotropic Material Model (i.e., Fiber-glass reinforced plastic pipe); the default coefficient of expansion is 12.0 E-6 in./in./°F. Material 21 indicates user-defined properties. Material numbers over 100 are from the Material Database and include the allowable stress and other piping code data.


12


CAESAR II Intersection Types CAESAR II Type B31.3 Type

1 Reinforced

Notes

Reinforced Fabricated Tee Used to lower SIFs Not a fitting Modified pipe

2 Unreinforced

Unreinforced Fabricated Tee

Routine intersection Not a fitting Modified pipe Usually the cheapest

3 Welded Tee

Welding Tee

Usually size-on-size Governed by B16.9 Usually the lowest SIF Usually expensive

4 Sweepolet

Welded-in Contour Insert

Sit-in" fitting Forged fittings on a pipe

5 Weldolet

Branch Welded on Fitting

"Sit-on" fitting Forged fittings on a pipe

6 Extruded

Extruded Welding Tee

Seldom used Used for thick wall manifolds Extruded from straight pipe


Sketch


13

Code Stresses Listed below are the Code Stress equations for the actual and allowable stresses used by CAESAR II. For the listed codes, the actual stress is defined by the left hand side of the equation and the allowable stress is defined by the right hand side. The CAESAR II load case label is also listed after the equation. Typically the load case recommendations made by CAESAR II are sufficient for code compliance. However, CAESAR II does not recommend occasional load cases. Occasional loads are unknown in origin and must be specified by the user. US Codes Longitudinal Pressure Stress - Slp Slp = PD0/4tn

code approximation

Slp = PDi2/(D02 - Di2)

code exact equation, CAESAR II default

Operating Stress - unless otherwise specified S = Slp + Fax/A + Sb

<

NA

(OPE)

Sl = Slp + 0.75 i Ma / Z

<

Sh

(SUS)

i Mc / Z

<

f [ 1.25 (Sc+Sh) - Sl ]

(EXP)

Slp + 0.75 i Ma / Z + 0.75 i Mb / Z

<

k Sh

(OCC)

Sl = Slp + Fax/A + Sb

<

Sh

(SUS)

sqrt (Sb2 + 4 St2)

<

f [ 1.25 (Sc+Sh) - Sl ]

(EXP)

Fax/A + Sb + Slp

<

k Sh

(OCC)

<

1.5 Sh

(SUS)

i Mc / Z

<

f (1.25 Sc + 0.25 Sh) + Sh -Sl

(EXP)

B1 * Slpmax + B2 * (Ma + Mb) / Z

<

1.8 Sh and < 1.5 Sy

(OCC)

B31.1

B31.3

Sb = [sqrt ( (iiMi)2 + (i0M0)2 )]/Z

ASME SECT III CLASS 2 & 3


14


B31.1 (1967) and Navy Section 505 Sl = Slp + sqrt (Sb2 + 4 St2)

<

Sh

(SUS)

sqrt ( Sb + 4 St )

<

f (1.25Sc + 0.25Sh + (Sh-Sl))

(EXP)

<

k Sh

(OCC)

<

0.9 (Syield)

(OPE)

2

2

Slp + sqrt (Sb + 4 St ) 2

2

B31.4 If FAC = 1.0 (fully restrained pipe) FAC | E dT -

SHOOP| + SHOOP

If FAC = 0.001 (buried, but soil restraints modeled) <

0.9 (Syield)

(OPE)

<

0.9 (Syield)

(OPE)

(Slp + Sb + Fax/A) (1.0 - FAC)

<

(0.75) (0.72) (Syield)

(SUS)

2

sqrt ( Sb + 4 St )

<

0.72 (Syield)

(EXP)


<

0.8 (Syield)

(OCC)

Fax/A -

SHOOP + Sb + SHOOP

(If Slp + Fax/A is compressive) If FAC = 0.0 (fully above ground) Slp + Fax/A + Sb + SHOOP (If Slp + Fax/A is compressive) 2

B31.4 Chapter IX Hoop Stress: Sh

(OPE, SUS, OCC)

F1 Sy

Longitudinal Stress: |SL| Equivalent Stress: Se

0.8 Sy

0.9 Sy

Where: Sy = specified minimum yield strength F1 = hoop stress design factor (0.60 or 0.72, see Table A402.3.5(a) of B31.4) Sh = (Pi – Pe) D / 2t SL= Sa + Sb or Sa - Sb, whichever results in greater stress value Se = 2[((SL - Sh)/2)2 + St2]1/2


(OPE, SUS, OCC) (OPE, SUS, OCC)


15

B31.5 Sl = Slp + Fax/A + Sb

<

Sh

(SUS)

sqrt (Sb + 4 St )

<

f [ 1.25 (Sc+Sh) - Sl ]

(EXP)

<

k Sh

(OCC)

2

2

Fax/A + Sb + Slp Sb = [sqrt ( (iiMi) + (i0M0) )]/Z 2

2

B31.8 B31.8 For Restrained Pipe (as defined in Section 833.1): For Straight Pipe:

Max(SL, SC)

< 0.9ST

(OPE)

Max(SL, SC)

< 0.9ST

(SUS)

SL

< 0.9ST

(OCC)*

< ST

(OCC) *

and SC

CAESAR II prints the controlling stress of the two SL = SP + SX + SB For All Other Components

SL

< 0.9ST

(OPE, SUS, OCC)

B31.8 For Unrestrained Pipe (as defined in Section 833.1): SL

< 0.75ST

(SUS, OCC)

SE

< f[1.25(SC + SH) – SL]

(EXP)

Where: SL

= SP + SX + SB

SP

= 0.3SHoop (for restrained pipe) = 0.5SHoop (for unrestrained pipe)

SX

= R/A

SB

= MB/Z (for straight pipe/bends with SIF = 1.0) = MR/Z (for other components)

SC MR Mt2]

= Max (|SHoop – SL|, sqrt[SL2 – SLSHoop + SHoop2]) = sqrt[(0.75iiMi)2 + (0.75ioMo)2 +

SE

= ME/Z

ME

= sqrt[(0.75iiMi)2 + (0.75ioMo)2 + Mt2]


16


B31.8 For Unrestrained Pipe (as defined in Section 833.1): Continued… S

= Specified Minimum Yield Stress

T

= Temperature Derating Factor

SH

= 0.33SUT

SC

= 0.33SU

SU

= Specified Minimum Ultimate Tensile Stress

B31.8 Chapter VIII Hoop Stress:

Sh

F1 S T

(OPE, SUS, OCC)

Longitudinal Stress:

|SL|

0.8 S

(OPE, SUS, OCC)

Equivalent Stress:

Se

0.9 S

(OPE, SUS, OCC)

Where: S = Specified Minimum Yield Strength F1= Hoop Stress Design Factor (0.50 or 0.72, see Table A842.22 of the B31.8 Code) T= Temperature Derating Factor (see Table 841.116A of the B31.8 Code) Note: The product of S and T (i.e. the yield stress at operating temperature) is required in SH of the CAESAR II Input.

Sh= (Pi – Pe) D / 2t SL = maximum longitudinal stress (positive tensile, negative compressive) Se = 2[((SL - Sh)/2)2 + Ss2]1/2 Ss = tangential shear stress GPTC Slp + 0.75i Ma/Z Sl = Slp+Sb Se = sqrt(Sb +4St ) 2

2

<

Syield

(OPE)

<

0.75(Sy)Ft

(SUS)

<

0.72 (Syield)

(EXP)

0.9 (Syield)

(OPE)

Note: GPTC is similar to B31.8 with noted changes.

B31.11 If FAC = 1.0 (fully restrained pipe) FAC | E

dT -

SHOOP| + SHOOP

<

If FAC = 0.001 (buried, but soil restraints modeled) Fax/A -

SHOOP + Sb + SHOOP

<

0.9 (Syield)


(OPE)


17

B31.11 Continued … (If Slp + Fax/A is compressive) If FAC = 0.0 (fully above ground) Slp + Fax/A + Sb + SHOOP

<

0.9 (Syield)

(OPE)


<

(0.75) (0.72) (Syield)

(SUS)

sqrt ( Sb2 + 4 St2 )

<

0.72 (Syield)

(EXP)


<

0.88 (Syield)

(OCC)

<

0.9 S * T

(OPE)

(If Slp + Fax/A is compressive)

International Codes Canadian Z662 If FAC = 1.0 (fully restrained pipe) |E

dT -

Sh| + Sh

If FAC = 0.001 (buried, but soil restraints modeled) <

S*T

(OPE)

<

S*T

(OPE)

Sl = 0.5Sh + Sb

<

S*F*L*T

(SUS, OCC)

SE = sqrt [Sb 2 + 4St2]

<

0.72 S * T

(EXP)

Slp + 0.75i Ma/Z

<

Sh

(SUS)

iMc/Z

<

f (1.25 Sc + .25 Sh) + Sh - Sl

(EXP)

Slpmax + 0.75i (Ma + Mb)/Z

<

1.2 Sh

(OCC)

|Fax / A -

Sh | + Sb + Sh

(If Fax / A -

Sh is compressive)

If FAC = 0.0 (fully above ground) |Slp + Fax / A| + Sb + Sh (If Slp + Fax / A is compressive)

RCC-M C & D

Stoomwezen Slp + 0.75i Ma/Z < iMc/Z <

f

(SUS)

fe

Slp + 0.75i (Ma + Mb)/Z <

(EXP) 1.2f


(OCC)

18


CODETI Sl = Slp + Fax/A + Sb

<

Sh

(SUS)

sqrt (Sb + 4St )

<

f [1.25 (Sl + Sh)] - Sl

(EXP)

<

Ksh

(OCC)

2

2

Slp + Fax/A + iMa/Z + iMb/Z Sb = [ Sqrt ((iiMi) + (i0M0) ] /Z 2

2

Norwegian (SUS)

2 PDi .75Ma SI = + 2 2 Z Eff(D0 D1 )

iMc/Z < Sh + Sr - Sl

(EXP)

.75i (Ma + Mb) PmaxDi2 + 2 2 Z Eff(D0 -Di )

(OCC)

M = sqrt (Mx2 + My2 + Mz2) Sr= Minimum of 1.25 Sc + 0.25 Sh; FrRs-F2; or Fr (1.25R1 + 0.25R2) The latter applies to temperatures over 370°C; 425°C for Austenitic stainless steel Fr= Cyclic reduction factor Rs= Permissible extent of stress for 7000 cycles R1= Minimum of Sc and 0.267 Rm R2= Minimum of Sh and 0.367 Rm Rm = Ultimate tensile strength at room temperature

FDBR

Sl = Slp + 0.75 i Ma / Z

<

Sh

(SUS)

i Mc / Z

<

f [ 1.25 (Sc+Sh) - Sl ]

(EXP)

Slp + 0.75 i Ma / Z + 0.75 i Mb / Z

<

k Sh

(OCC)



19

BS 7159 If Sx is tensile:

<

Sh

(OPE)

<

Sh*EH/EA

(OPE)

<

Sh*EH/EA

(OPE)

<

1.25Sh

(OPE)

2 2 sqrt (Sx + 4Ss )

and 2 2 sqrt (S + 4Ss )

or, if Sx is compressive: S +

x Sx

and Sx Sx =

( ) + [sqrt((i xi Mi ) 2 +(i xo M o )2 )] Z ( 4t )

P Dm

( ) - [sqrt((i xi Mi ) 2 +(i xo M o ) 2 )] - Fx A Z ( 4t )

P Dm

(If Fx/A > P(Dm)/(4t), and it is compressive) S =

=

=

( ) ( 2t )

for straight pipes

MP D m

( ) [sqrt((i i Mi )2 +(i + Z ( 2t )

MP D m

2 o M o ) )]

( ) + [sqrt((i xi Mi ) 2 +(i xo M o )2 )] Z ( 2t )

MP D m

for bends

for tees

Dm and t are always for the Run Pipe Eff = Ratio of E to Ex


20


UKOOA ab (f2/r) + PDm/ (4t) < (f1 f2 LTHS) / 2.0 Where: P = design pressure Dm = pipe mean diameter t = pipe wall thickness f1 = factor of safety for 97.5% lower confidence limit, usually 0.85 f2 = system factory of safety, usually 0.67 ab = axial bending stress due to mechanical loads r = a(0:1) / a(2:1) a(0:1) = long term axial tensile strength in absence of pressure load a(2:1) = long term axial tensile strength in under only pressure loading LTHS = long term hydrostatic strength (hoop stress allowable) BS 806 Straight Pipe fc

=

sqrt(F2 + 4fs2)

fs

=

Mt(d + 2t) / 4I

F

=

max (ft, fL)

ft

=

pd/2t + 0.5p

fL

=

pd2/[4t(d + t)] + (d + 2t)[sqrt(mi2 + mo2)] / 2I

<

SAOPE

<

SASUS

<

SAEXP

<

SAOPE

<

SASUS

<

SAEXP

Bends fc

=

sqrt (F2 + 4 fs2)

fs

=

Mt (d + 2t) /4I

F

=

max (ft, fL)

ft

=

r/I * sqrt[(miFTi)2 + (m0FTo)2]

fs

=

r/I * sqrt[(miFLi)2 + (m0FLo)2]



21

BS 806 Continued … Branch Junctions fcb

=

q * sqrt[fb2 + 4fsb2]

fb

=

(d + t)*p*m/(2t) + r/I*sqrt[(miFTL)2 + (moFTO)2]

Fsb

=

Mt (d + 2t) / 4I

q

= 1.0 except for operating cases = 5 or .44 bases on d2/d1 ratio in operating cases

m

=

<

SAOPE

<

SASUS

<

SAEXP

geometric parameter

EXP SA =

min[(H*Sproof ambient + H*Sproof design); (H*Sproof ambient + F)]

OPE SA =

Savg rupture at design temperature

SUS SA =

min[.8*Sproof, Screep rupture]

Det Norske Veritas (DNV) Hoop Stress: Sh

ns SMYS

Hoop Stress: Sh

nu SMTS

Longitudinal Stress: SL

n SMYS

Equivalent Stress: Se n SMYS Where: Sh

=

(Pi – Pe) (D – t) / 2t

ns

=

hoop stress yield usage factor Tables C1 and C2 of DNV

SMYS nu

= =

SMTS

specified minimum yield strength, at operating temperature hoop stress bursting usage factor Tables C1 and C2 of DNV

=

specified minimum tensile strength, at operating temperature

SL

=

maximum longitudinal stress

n

=

equivalent stress usage factor Table C4 of DNV

Se

=

[Sh2 + SL2 - ShSL + 3t2]1/2


22


EN-13480 <

Kfn

(SUS)

<

fn + fh

(EXP)

<

Kfn

(OCC)

EN-13480 Alternate Option due to primary loads

<

Kfn

(SUS)

<

fn + fh

(EXP)

<

Kfn

(OCC)

due to occasional loads

PD8010 Part 1 Hoop Stress

Sh< aeSy

(OPE, SUS, OCC)

Equivalent Stress

Se< 0.9Sy

(OPE, SUS, OCC)

Where: Sy

= specified minimum yield strength

e

= weld joint factor

a

= design factor

Sh Se www.cadfamily.com EMail:[email protected] The document is for study only,if tort to your rights,please inform us,we will delete


23

PD8010 Part 1 Continued … hoop stress using nominal dimensions

Shl ST = SL

Based on restrained/unrestrained status

SL for unrestrained piping SL for restrained piping If FAC = 1.0 (fully restrained pipe) 0.9 (Syield)

(OPE)

<

0.9 (Syield)

(OPE)

<

0.9 (Syield)

(OPE)


<

(0.75) (0.72) (Syield)

(SUS)

sqrt ( Sb2 + 4 St2 )

<

0.72 (Syield)

(EXP)


<

0.8 (Syield)

(OCC)

FAC | E

dT - SHOOP| + SHOOP

<

If FAC = 0.001 (buried, but soil restraints modeled) Fax/A -

SHOOP + Sb + SHOOP

(If Slp + Fax/A is compressive) If FAC = 0.0 (fully above ground) Slp + Fax/A + Sb + SHOOP (If Slp + Fax/A is compressive)

PD8010 Part 2 Hoop Stress

Sh< fdhSy

(OPE, SUS, OCC)

Equivalent Stress

Se< fdeSy

(OPE, SUS, OCC)

Where: Sy

specified minimum yield strength

fdh

hoop stress design factor (See Table 2)

fde

equivalent stress design factor (See Table 2)

Sh= S e= ST =


24


Node Locations on Bends Bends are defined by the element entering the bend and the element leaving the bend. The actual bend curvature is always physically at the TO end of the element entering the bend. The element leaving a bend must appear immediately after the element defining (entering) the bend. The default bend radius is 1.5 times the pipe nominal OD. For stress and displacement output the TO node of the element entering the bend is located geometrically at the FAR point on the bend. The FAR point is at the weld line of the bend, and adjacent to the straight element leaving the bend. The NEAR point on the bend is at the weld line of the bend, and adjacent to the straight element entering the bend. The FROM point on the element is located at the NEAR point of the bend if the total length of the element as specified in the DX, DY and DZ fields is equal to: Radius * tan( Beta / 2 ) where “Beta” is the bend angle, and Radius is the bend radius of curvature to the bend centerline. Nodes defined in the Angle # and Node # fields are placed at the given angle on the bend curvature. The angle starts with zero degrees at the NEAR point on the bend and goes to “Beta” degrees at the FAR point of the bend. Angles are always entered in degrees. By default, nodes on the bend curvature cannot be specified within five (5) degrees of one another or within five degrees of the nearest end point. This and other bend settings may be changed through the Main Menu, Configure-Setup processor. When the FROM node on the element entering the bend is not at the bend NEAR point a node may be placed at the near point of the bend by entering an Angle # on the bend spreadsheet equal to 0.0 degrees. For more information see the following figure. When defining a bend element for the first time in the pipe spreadsheet, nodes are automatically placed at the near and mid point of the bend. The generated midpoint node number is one less than the TO node number on the element, and the generated near point node number is two less than the TO node number on the element. A near point should always be included in the model in tight, highly formed piping systems. The top-left figure below shows the points on the bend as they would be input. The top-right figure shows the actual geometric location of the points on the bend. The bottom-left figure shows the same geometry except that two nodes are defined on the bend curvature at angles of zero and forty-five degrees.



25

For an animated tutorial on modeling bends, select the ANIMATED TUTORIALS option on the Help menu.


26


CAESAR II Quality Assurance Manual The CAESAR II Quality Assurance Manual is intended to serve as a publicly available verification document. This manual discusses (briefly) the current industry QA standards, the COADE QA standard, a series of benchmark jobs, and instructions for users implementing QA procedures on their own hardware. The benchmark jobs consist of comparisons to published data by ASME and the NRC. Additional test jobs compare CAESAR II results to other industry programs. For additional information on the Quality Assurance Manual, please contact the sales department at [email protected]. Mechanical Engineering News As an aid to the users of COADE software products, COADE publishes Mechanical Engineering News several times a year. This publication contains discussions on recent developments that affect users, and technical features illustrating modeling techniques and software applications. This newsletter is sent to all users of COADE software at the time of publication. Back issues can be acquired by contacting the COADE sales staff. Additional COADE Software Programs CADWorx Plant - An AutoCAD based plant design/drafting program with a bidirectional data transfer link to CAESAR II. CADWorx allows models to be created in ortho, iso, 2D or 3D modes. CADWorx template specifications, contained with

built in auto routing, auto iso, stress iso, auto dimensioning, complete libraries, center of gravity calculations, and bill of materials, provides the most complete plant design package to designers. CodeCalc - A program for the design or analysis of pressure vessel components. CodeCalc capabilities include: analysis of tubesheets, rectangular vessels, flanges, nozzles, Zick Analysis, and the standard internal/external thickness and pressure computations on heads, shells, and cones. API 579 calculations are also included. PV Elite - A comprehensive program for the design or analysis of vertical and horizontal vessels. Pressure Vessel Codes include ASME VIII-1 and VIII-2, PD:5500 and EN-13445. PVElite includes all of the CodeCalc functionality. TANK - A program for the design or rerating of API-650/653 storage tanks. The program includes API 650 Appendices A, E, F, M, P, and S, as well as API 653 Appendix B. Computations address: winds girders, conical roof design, allowed fluid heights, and remaining corrosion allowance. www.cadfamily.com EMail:[email protected] The document is for study only,if tort to your rights,please inform us,we will delete

Index

1

Quick Reference Guide Index A

I

Additional COADE Software Programs • 26 ASME SECT III CLASS 2 & 3 • 13

International Stresses • 17

B

List of Materials • 11

B31.1 • 13 B31.1 (1967) and Navy Section 505 • 14 B31.11 • 16, 17 B31.3 • 13 B31.4 • 14 B31.4 Chapter IX • 14 B31.5 • 15 B31.8 • 15 B31.8 Chapter VIII • 16 Bends • 20 Branch Junctions • 21 BS 7159 • 19 BS 806 • 20, 21 C CAESAR II Interfaces • 3 CAESAR II Intersection Types • 12 CAESAR II Pipe Stress Seminars • 2 CAESAR II Quality Assurance Manual • 26 CAESAR II Quick Reference Guide Version 5.10 • 1 CAESAR II Software • 2 Canadian Z662 • 17 Code Stresses • 13 CODETI • 18 Computation Control • 6 D Database Definitions • 9 Det Norske Veritas (DNV) • 21

L M Mechanical Engineering News • 26 Miscellaneous Computations • 10 N Node Locations on Bends • 24 Norwegian • 18 P Piping Codes • 4 Plot Colors • 8 R RCC-M C & D • 17 Restraints • 5 S Setup File Directives List • 6 SIFS and Stresses • 7 Stoomwezen • 17 System Requirements • 3 T Troubleshooting • 3 U UKOOA • 20 US Codes • 13

E EN-13480 • 22 F FDBR • 18 G Geometry Directives • 6 GPTC • 16


COADE Inc. 12777 Jones Road Suite 480 Houston, Texas 77070 Phone: (281)890-4566 Fax: (281)890-3301 Email: [email protected] Web: www.coade.com

CAESAR II Quick Reference Guide Version 5.10 Last Revised 111/2007


CAESAR II Quick Reference Guide

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