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Unformatted text preview: expansion fan doing the turning, relative to the nozzle centerline. e. Determine the Mach number and temperature of the flow after this initial turn. 3. A flat plate airfoil is placed in a supersonic wind tunnel at an angle of attack of 18 degrees. The uniform air flow approaching the airfoil is generated by a nozzle with an exit to throat area ration of 5.3 exhausting air from a chamber where the tempera...
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