Question: Consider a Mach 3.6 supersonic airflow over a compression corner with a deflection angle of 15, the wave angle is = 28.57 . The specific

Consider a Mach 3.6 supersonic airflow over a compression corner with a deflection angle of 15, the wave angle is = 28.57 . The specific heat capacity ratio is = 1.38. If the deflection angle is doubled to 30, the wave angle is = 46.64. what is the increase in shock strength? Is it also doubled? Only consider weak solutions

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