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Question

A cantilever beam is shown in the figure. The moment to be applied at free end for zero vertical deflection at the point is

A
9kNm clockwise
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B
9kNm anti-clockwise
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C
12kNm clockwise
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D
12kNm anti-clockwise
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Solution

The correct option is C 12kNm clockwise

Deflection due to 9kN will be


Moment should be applied as shown:

Deflection due to applied moment will be:


Writing deflection compatibility equation at free end for deflection to be zero:
δ1=δ2
9×233EI=M×222EI
M=9×2×23
M=12kNm (clockwise)

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