Introduction to Mechanics of Deformable Solids |
From inside the book
Results 1-3 of 70
Page 87
Do you need to know the answer to Prob . 5 . 2 first ? B . Compute the change in
wall thickness . C . Compute the change in interior volume . 5 . 4 What is the
factor of safety against rupture in Prob . 5 . 2 ? Take necking or local thinning into
...
Do you need to know the answer to Prob . 5 . 2 first ? B . Compute the change in
wall thickness . C . Compute the change in interior volume . 5 . 4 What is the
factor of safety against rupture in Prob . 5 . 2 ? Take necking or local thinning into
...
Page 88
5.10 Find a reasonable answer for the change in diameter and the change in
length in 1 year of a pipe 12 ft long , 6 in . in diameter , t - in . wall , with 600 psi
interior pressure . ( Use Figs . 3.3 , 5.7 , 5.8 as best you can . ) A. OFHC copper at
165 ...
5.10 Find a reasonable answer for the change in diameter and the change in
length in 1 year of a pipe 12 ft long , 6 in . in diameter , t - in . wall , with 600 psi
interior pressure . ( Use Figs . 3.3 , 5.7 , 5.8 as best you can . ) A. OFHC copper at
165 ...
Page 399
5 : 9 ) and so is a better answer . For M6 > 17M6 , ( 15 . 5 : 9 ) gives the actual
limit load , and Fig . 15 . 9a is the correct collapse configuration . Although ( 15 . 5
: 10 ) gives a better answer than ( 15 . 5 : 9 ) when MTM < 17MÁ , it is not the best
...
5 : 9 ) and so is a better answer . For M6 > 17M6 , ( 15 . 5 : 9 ) gives the actual
limit load , and Fig . 15 . 9a is the correct collapse configuration . Although ( 15 . 5
: 10 ) gives a better answer than ( 15 . 5 : 9 ) when MTM < 17MÁ , it is not the best
...
What people are saying - Write a review
We haven't found any reviews in the usual places.
Other editions - View all
Common terms and phrases
actual addition angle answer applied assemblage axes axial axis beam behavior bending circle circular column combined compatibility components compression compressive stress Consider constant creep cross section curve cylinder deflection deformation determined diameter direction displacement effect elastic equal equation equilibrium example Figure Find force given gives homogeneous idealization increase initial interior isotropic length limit linear linear-elastic load material maximum Maxwell modulus moment needed nonlinear normal obtained outer plane plastic positive pressure principal Prob problem produced pure radius range ratio relation replaced requires residual response result rotation shaft shear stress shell shown shows simple sketch solid solution steel strain stress-strain relations structural Suppose surface symmetry temperature tensile tension thickness thin-walled torsion tube twisting uniform unloading versus viscous yield zero