Q2. Show that p = Cr² (α = 0 + sin cos 0 - tan a cos² 0) is a permissible Airy 1 function for the tapered cantilever of uniform thickness, shown in Figure 2, and derive expressions for the corresponding stresses or, de and Tre. Also, find the value of the radial stress at 0=0° when a=30°. w/ unit length Figure 2 a 0 r

Q2. Show that p = Cr² (α = 0 + sin cos 0 - tan a cos² 0) is a permissible Airy 1 function for the tapered cantilever of uniform thickness, shown in Figure 2, and derive expressions for the corresponding stresses or, de and Tre. Also, find the value of the radial stress at 0=0° when a=30°. w/ unit length Figure 2 a 0 r

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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