A pressurized steel tank is constructed with a helical weld that makes an angle at = 55" with the longitudinal axis (see figure). The tank has radius r = 0.6 m, wall thickness t = 18 mm, and internal pressure p = 2.8 MPa. Also, the steel has modulus of elasticity E = 200 GPa and Poisson's ratio v = 0.30. Determine the following quantities for the cylindrical part of the tank.(a) The circumferential and longitudinal stresses.(b) The maximum in-plane and out-of-plane shear stresses.(c) The circumferential and longitudinal strains.(d) The normal and shear stresses acting on planes parallel and perpendicular to the weld (show these stresses on a properly oriented stress element
A pressurized steel tank is constructed with a helical weld that makes an angle at = 55" with the longitudinal axis (see figure). The tank has radius r = 0.6 m, wall thickness t = 18 mm, and internal pressure p = 2.8 MPa. Also, the steel has modulus of elasticity E = 200 GPa and Poisson's ratio v = 0.30. Determine the following quantities for the cylindrical part of the tank.(a) The circumferential and longitudinal stresses.(b) The maximum in-plane and out-of-plane shear stresses.(c) The circumferential and longitudinal strains.(d) The normal and shear stresses acting on planes parallel and perpendicular to the weld (show these stresses on a properly oriented stress element
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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A pressurized steel tank is constructed with a helical weld that makes an angle at = 55" with the longitudinal axis (see figure). The tank has radius r = 0.6 m, wall thickness t = 18 mm, and internal pressure p = 2.8 MPa. Also, the steel has modulus of elasticity E = 200 GPa and Poisson's ratio v = 0.30. Determine the following quantities for the cylindrical part of the tank.
(a) The circumferential and longitudinal stresses.
(b) The maximum in-plane and out-of-plane shear stresses.
(c) The circumferential and longitudinal strains.
(d) The normal and shear stresses acting on planes parallel and perpendicular to the weld (show these stresses on a properly oriented stress element
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