1.

Find the velocity for minimum thrust required at steady level flight if wing loading is 75N/m2 and induced drag factor K is 0.0025. Consider CD0 as 0.02 and density as sea level.

A. 6.45m/s
B. 97m/s
C. 120m/s
D. 75m/s
Answer» B. 97m/s


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