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What is Oblique Shock and Expansion Waves Analysis about?

Here are the key steps to solve this problem: 1. The flow encounters an oblique shock at the leading edge, deflecting the flow by the angle α + ε = 25°. Calculate the post-shock Mach number and properties using oblique shock relations. 2. The flow then expands around the sides of the wedge through an expansion fan with deflection angle ε on each side. Calculate the post-expansion Mach number and properties. 3. The flow encounters another oblique shock at the trailing edge, turning the flow back to the f

Author

larison09

Language

EN