Estimate the required tail-setting angle

Reference no: EM131515246

Question: An airplane weighing 100 kN is 24.4 m in span. Its tailplane, which has a symmetrical section and is located 15.2 m behind the center of pressure of the wing, is required to exert zero pitching moment at a speed of 67 ms-1. Estimate the required tail-setting angle assuming elliptic loading on the wings.

Reference no: EM131515246

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