During an engine test on the ground, a propeller thrust T 5 3000 N is generated on the
Chapter 3, Problem 3/52(choose chapter or problem)
During an engine test on the ground, a propeller thrust T = 3000 N is generated on the 1800-kg airplane with mass center at G. The main wheels at B are locked and do not skid; the small tail wheel at A has no brake. Compute the percent change n in the normal forces at A and B as compared with their “engine-off ” values.
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