Question: ( b ) Triangular wedge in supersonic flow 4 . Consider a supersonic flow over a wedge with a half angle of 7 at an

(b) Triangular wedge in supersonic flow
4. Consider a supersonic flow over a wedge with a half angle of 7 at an angle of attack of 10 as shown in Figure 1b. Sketch the flow pattern before starting your analysis. Find coefficient of lift CL and coefficient of drag CD for an incoming flow at Mach 7. Neglect back drag. Use NACA Report 1135 charts.
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( b ) Triangular wedge in supersonic flow 4 .

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