3. A force P is applied to the rigid lever arm ABC as shown. The arm rotates counterclockwise about pinA through an angle of 0.06. Calculate the normal strain developed in wire BD.Answer:0.0014 mm/mm300 mm400 mm-4. The control linkage of an airplane consists of a rigid member DBC and a flexible cable AB. A force P isapplied to the end D of the member and causes it to rotate by 8-0.35°. The cable is assumed to beoriginally unstretched. Determine the strain developed in the cable.Answer: A = 0.00282 mm/mm

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3. A force P is applied to the rigid lever arm ABC as shown. The arm rotates counterclockwise about pin A through an angle of 0.06. Calculate the normal strain developed in wire BD. Answer: 0.0014 mm/mm 00 mm 2 400 mm-

3. A force P is applied to the rigid lever arm ABC as shown. The arm rotates counterclockwise about pin A through an angle of 0.06. Calculate the normal strain developed in wire BD. Answer: 0.0014 mm/mm 00 mm 2 400 mm-

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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Question

3. A force P is applied to the rigid lever arm ABC as shown. The arm rotates counterclockwise about pin
A through an angle of 0.06. Calculate the normal strain developed in wire BD.
Answer:
0.0014 mm/mm
300 mm
400 mm-
4. The control linkage of an airplane consists of a rigid member DBC and a flexible cable AB. A force P is
applied to the end D of the member and causes it to rotate by 8-0.35°. The cable is assumed to be
originally unstretched. Determine the strain developed in the cable.
Answer: A = 0.00282 mm/mm

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