Question #116428
An aircraft weighting 156960 N is powered by a jet engine whose thrust is independent of flight speed. The maximum rate of climb at sea level occurs at 152.5 m/s. The wing area is 46 m2. The drag polar is given by
1
Expert's answer
2020-06-10T07:51:03-0400

The drag polar is given by

CD = 0.016 + 0.045CL2

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