*2-8 Part of a control linkage for an a rigid member CBD and a flexible cab applied to the end D of the member an by -0.3°, determine the normal s Originally the cable is unstretched. 2-9 Part of a control linkage for an a rigid member CBD and a flexible cab applied to the end D of the member a strain in the cable of 0.0035 mm/mm, placement of point D. Originally the c Fo D

Structural Analysis
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Chapter2: Loads On Structures
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*2-8 Part of a control linkage for an airplane consists of a
rigid member CBD and a flexible cable AB. If a force is
applied to the end D of the member and causes it to rotate
by 0.3°, determine the normal strain in the cable.
Originally the cable is unstretched.
2-9 Part of a control linkage for an airplane consists of a
rigid member CBD and a flexible cable AB. If a force is
applied to the end D of the member and causes a normal
strain in the cable of 0.0035 mm/mm, determine the dis-
placement of point D. Originally the cable is unstretched.
Fo
A
400 mm-
D
R
300 mm
300 mm
P
Transcribed Image Text:*2-8 Part of a control linkage for an airplane consists of a rigid member CBD and a flexible cable AB. If a force is applied to the end D of the member and causes it to rotate by 0.3°, determine the normal strain in the cable. Originally the cable is unstretched. 2-9 Part of a control linkage for an airplane consists of a rigid member CBD and a flexible cable AB. If a force is applied to the end D of the member and causes a normal strain in the cable of 0.0035 mm/mm, determine the dis- placement of point D. Originally the cable is unstretched. Fo A 400 mm- D R 300 mm 300 mm P
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