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Question: chapter s3 problem 3048 the cargo door for an airplane...

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Chapter S3, Problem $3/048 The cargo door for an airplane of circular fuselage section consists of the uniform semicircular cowling AB of mass m. Determine the compression C in the horizontal strut at B to hold the door open in the position shown. Also find the total force FA supported by the hinge at A. (Consult Table D/3 of Appendix D for the position of the centroid or mass center of the cowling.) -. Horiz Light strut Closed position of B Answers C- mg mg Click if you would like to Show Work for this question: Open Show Work
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