3. The material is subjected to biaxial loading producing uniform normal stress ox and o, asshown. The strains are e, = -0.00065 and e, = -0.00040. Use E = 207 GPa and v = 0.35.Determine the following:(a) oz. Indicate tension or compression. Use 2 decimal places.(b) ơy. Indicate tension or compression. Use 2 decimal places.(c) Change in the thickness of the material. Indicate elongation or contraction. Use 5decimal places and scientific notation of x 10-3 (Example: .(25 pts)x 10-3)yOyx.Oyt = 16 mm

Answered: Image /qna-images/answer/faa97aeb-74ea-44fb-855e-c264a7ee3e12.jpg

3. The material is subjected to biaxial loading producing uniform normal stress ox and oy as shown. The strains are e = -0.00065 and e, = -0.00040. Use E = 207 GPa and v = 0.35. Determine the following: (a) oy. Indicate tension or compression. Use 2 decimal places. (b) oy. Indicate tension or compression. Use 2 decimal places. (c) Change in the thickness of the material. Indicate elongation or contraction. Use 5 decimal places and scientific notation of x 10-3 (Example:_ (25 pts) x 10-3) y Oy Ox Oy At = 16 mm

3. The material is subjected to biaxial loading producing uniform normal stress ox and oy as shown. The strains are e = -0.00065 and e, = -0.00040. Use E = 207 GPa and v = 0.35. Determine the following: (a) oy. Indicate tension or compression. Use 2 decimal places. (b) oy. Indicate tension or compression. Use 2 decimal places. (c) Change in the thickness of the material. Indicate elongation or contraction. Use 5 decimal places and scientific notation of x 10-3 (Example:_ (25 pts) x 10-3) y Oy Ox Oy At = 16 mm

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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