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<- Useful page 2 formula
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Nozzle Loads WRC 107 Ver 1.1
17-Feb-13
Page 1 of 1
Megyesy's Pressure Vessel Handbook
Verification Calc #1
Megyesy PV Book 11th Ed. P153
<- vessel
<- Nozzle
F
Ro
Inputs:
9.250 <- Shell Midline Radius (Rm)
4.313 <- Nozzle Outside Radius (Ro)
0.750 <- Shell Thickness (T)
8
9
T
10
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40,000 <- F (Load, lbs)
662 <- Mc (moment, in.lbs)
662 <- Ml (moment, in.lbs)
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Mrlm
Mrcm
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150 <- P
36,000 <- Sy (Yield strength)
16,600 <- Sa (Allowable Stress)
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Constants:
Beta
Gamma
Alpha
Sigma
Delta
Calculated stress
Max stress
= (2P/t)*(Rm-T/2)
= Sa
29
Maximum Allowed Loads (uncombined):
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end load
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Mrcm = (Rm^2*Ro*Sy)/(Sigma)
= (9.25^2*4.3125*36000)/(95)
= 140,302
in.lbs
(Allowed at Fmax and Ml = 0)
Moment l
Mrlm = (Rm^2*Ro/Delta)*(Sy-Stress)
= (9.25^2*4.3125/43)*(36000-3550)
= 279,698
in.lbs
(Allowed at Fmax and Mc = 0)
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(Allowed at Mc and Ml = 0)
Moment c
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Fmax = (Rm^2/alpha)*(Sy-Stress)
= (9.25^2/58)*(36000-3550)
= 47,555
lbs
= 0.875(Ro/Rm)
= Rm/T
(Interpolated)
(Interpolated)
(Interpolated)
= 3,550
= 16,600
Combined Loads:
F/Fmax = 40000 / 47555
Mc/Mrcm = 662 / 140302
Ml/Mrlm = 662 / 279698
F/Fmax = 0.841
Mc/Mrcm = 0.005
Mc/Mrcm = 0.002
Total Load = 0.848
= 84.8%
Okay
=
=
=
=
=
=
0.408
12
58
95
43
3,550
RM
1
Nozzle Loads WRC 107
Written By: Laurence Brundrett
Code: Megyessy "Pressure Vessel Handbook", 11th Edition
Addenda:
Sections: Pages 153 - 157
Update Log
Date
24-May-99
24-May-00
2-Jul-00
3-Aug-00
Change
Verified against Megyessy sample Volume 11 pages 153 - 154
Hand Calculated for Audit
Hand Calculation against example in Megyesy's book
Further Hand Calculations - posted set - changed method of calculating total loa
Added Commentary, Legal
Locked Cells - Password = "100"
3-Oct-00 Updated to A2000 format
New print macro
New legal statement
Version Number assigned = 1.1
Checked Against previous verification calcs
Locked Cells - Password = "100"
d
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