The cross-section area distribution along the x-direction of the body axis of a thin wing-body assembly is given as where V is the volume of the combination, upper S left parenthesis x right upper S left parenthesis x right parenthesis upper S left parenthesis x right parenthesisis the cross-sectional area of the combination at x, L is the length of the combination, Try to find the zero-lift shock wave drag of the combination at 

Transcribed Image Text:

64(V)(x 450-4-(-2)-(1-2) dS(x) dx L L