A uniform supersonic airflow traveling at passes over a wedge (as Figure). An oblique shock, making...

A uniform supersonic airflow traveling at passes over a wedge (as Figure). An oblique shock, making an angle of 40° with the flow direction, is attached to the wedge under these flow conditions. If the static pressure and temperature in the uniform flow are 20k Pa, -10 °C, respectively. Determine the static pressure and temperature behind the wave, the Mach number of the flow passing over the wedge, and the wedge half-angle.

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samet mamat answered 7 months ago

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As shown in the Figure below, a light string that does not stretch changes from horizontal to vertical as it passes over the edge of a table.

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A uniform supersonic airflow traveling at passes over a wedge (as Figure). An oblique shock, making...

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An airliner passes over an airport at noon traveling 510 mi divided by hr due west....

As shown in the Figure below, a light string that does not stretch changes from horizontal to vertical as it passes over the edge of a table.