Problem 1. In a test on an aerosol can it was loaded to a gage pressure p = 69.0 psi.While pressurized, the can is also subjected to a tensile axial load N = 400 lb and atorque T = 250 in - lb. The can has 3.0 in diameter and wall thickness t = 0.006 in. Thecross-sectional area of the wall (thin ring) is A = 2rt and the polar moment of inertia ofthe wall (thin ring) with respect to the centroid is J= 2r°t. The maximum shear stressTron the surface is t=-JNTT.XThe blue point on the surface of the aerosol can has its sides parallel and perpendicularto the can's longitudinal axis (x). Determine magnitudes of normal and shear stressesacting on the blue point.Ox = OL =oy = OH =.Sketch the stresses with their correct senses on the enlarged view of the blue pointbelow.

inside pressure p=69 psinormal load N=400 lb and torque T=250 lb-indiameter d=3.0 in and radiud…

Problem 1. In a test on an aerosol can it was loaded to a gage pressure p = 69.0 psi. While pressurized, the can is also subjected to a tensile axial load N = 400 lb and a torque T= 250 in - Ib. The can has 3.0 in diameter and wall thickness t = 0.006 in. The cross-sectional area of the wall (thin ring) is A = 2rrt and the polar moment of inertia of the wall (thin ring) with respect to the centroid is J= 2rr't. The maximum shear stress Tr on the surface is t=- J N T N The blue point on the surface of the aerosol can has its sides parallel and perpendicular to the can's longitudinal axis (x). Determine magnitudes of normal and shear stresses acting on the blue point. O, =0 =- Sketch the stresses with their correct senses on the enlarged view of the blue point below.

Problem 1. In a test on an aerosol can it was loaded to a gage pressure p = 69.0 psi. While pressurized, the can is also subjected to a tensile axial load N = 400 lb and a torque T= 250 in - Ib. The can has 3.0 in diameter and wall thickness t = 0.006 in. The cross-sectional area of the wall (thin ring) is A = 2rrt and the polar moment of inertia of the wall (thin ring) with respect to the centroid is J= 2rr't. The maximum shear stress Tr on the surface is t=- J N T N The blue point on the surface of the aerosol can has its sides parallel and perpendicular to the can's longitudinal axis (x). Determine magnitudes of normal and shear stresses acting on the blue point. O, =0 =- Sketch the stresses with their correct senses on the enlarged view of the blue point below.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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Concept explainers

Temperature Difference and Heat Transfer

Whenever there is a flow of heat flux resulting from a temperature gradient within the material or between two materials, there is heat transfer. Heat transfer primarily arises due to temperature differences between two bodies or within bodies. The term temperature gradient denotes temperature differences or variation of temperature due to change in some quantity. The fundamental use of the concept of temperature is found in the zeroth law of thermodynamics.

Question

Problem 1. In a test on an aerosol can it was loaded to a gage pressure p = 69.0 psi.
While pressurized, the can is also subjected to a tensile axial load N = 400 lb and a
torque T = 250 in - lb. The can has 3.0 in diameter and wall thickness t = 0.006 in. The
cross-sectional area of the wall (thin ring) is A = 2rt and the polar moment of inertia of
the wall (thin ring) with respect to the centroid is J= 2r°t. The maximum shear stress
Tr
on the surface is t=-
J
N
T
T.
X
The blue point on the surface of the aerosol can has its sides parallel and perpendicular
to the can's longitudinal axis (x). Determine magnitudes of normal and shear stresses
acting on the blue point.
Ox = OL =
oy = OH =.
Sketch the stresses with their correct senses on the enlarged view of the blue point
below.

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