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Unformatted text preview: convex corner which turns the flow by 30 degrees. a. Calculate the Mach number after the turn and the pressure and stagnation pressure here. b. Determine the angle of the leading and trailing edges of the expansion fan, relative to the initial flow direction c. Determine the angle of the flow at a point in the expansion fan where the flow has reached Mach 3. What will be the shape and angle(s) of the region in the wave where the Mach number is 3? d. In the second test, the same flow encounters a gradual concave turn. The flow temperature after...
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This document was uploaded on 02/20/2014.
- Spring '14