An air flow with a mach number of 8 is deflected by a wedge


1. An air flow with a Mach number of 2.0 passes through an oblique shock wave inclined at an angle of 45° . Find the flow deflection angle α.

2. An air flow with a Mach number of 8 is deflected by a wedge through an angle α. What is the maximum value of α for an attached oblique shock?

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Chemistry: An air flow with a mach number of 8 is deflected by a wedge
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