1.

Cambered wing has minimum drag coefficient of 0.05 and constant K of 0.023. If CL is 0.8 then find the value of CD. Given minimum drag occurs at CL of 0.1.

A. 0.06127
B. 6.1
C. 61.2
D. 0.6721
Answer» B. 6.1


Discussion

No Comment Found