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Determine the largest (allowable) compressive loadP (in kN) that can be supported by the aluminum cylinder with a diameter of 200 mm if the failure shear stress along the plane through section a-a is tfail = 20 MPa with a factor of safety for shear of F.S. = 2.3. a 25° 200 mm

Determine the largest (allowable) compressive loadP (in kN) that can be supported by the aluminum cylinder with a diameter of 200 mm if the failure shear stress along the plane through section a-a is tfail = 20 MPa with a factor of safety for shear of F.S. = 2.3. a 25° 200 mm

Structural Analysis
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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How would the largest allow compressive load P that can be supported by the aluminum cylinder be determined for this problem?

Determine the largest (allowable) compressive load P (in kN) that can be supported by the aluminum cylinder with a diameter of 200 mm if the failure shear stress along the plane through section a-a is tfail = 20 MPa with a factor of safety for shear of F.S. = 2.3. a 25° a 200 mm
Transcribed Image Text:Determine the largest (allowable) compressive load P (in kN) that can be supported by the aluminum cylinder with a diameter of 200 mm if the failure shear stress along the plane through section a-a is tfail = 20 MPa with a factor of safety for shear of F.S. = 2.3. a 25° a 200 mm
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Diameter of cyinder, D =200mmangle of plane aa with horizontal =25°Load applied =PFactor of safety, FOS = 2.3Faiure shear stress, τf =20MPa.

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