1.

Which of these equations is used for computing the lift and wave drag over a supersonic airfoil?

A. C<sub>p</sub>= ( frac {2 }{ sqrt {M_ ^2-1}} )
B. C<sub>p</sub>= ( frac {2 }{ sqrt {M_ ^2+1}} )
C. C<sub>p</sub>= ( frac { sqrt {M_ ^2-1}}{ } )
D. C<sub>p</sub>= ( frac { sqrt {M_ ^2+1}}{ } )
Answer» B. C<sub>p</sub>= ( frac {2 }{ sqrt {M_ ^2+1}} )


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