Consider a wedge with a half-angle of 10° flying at Mach 2
Consider a wedge with a half-angle of 10° flying at Mach 2. The oblique shock wave angle \beta is 38.4 10 41.5 39.3 The Correct Answer and Explanation is: Correct Answer: 39.3° Explanation: In compressible flow, when a supersonic flow encounters a wedge, an oblique shock wave forms ahead of the wedge. The angle this […]
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