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sure recovery when the at Ax/A, 1.2, i.e. th

sure recovery when the at Ax/A, 1.2, i.e. th

Question
(a) inlet total pressure recovery with the shock at the lip, i.e. the best backpressure da an obomm (b) inlet total pressure recovery when the shock is inside the duct at A,/A, = 1.2, i.e. the super- critical mode M (@) (C) inlet total pressure recovery in subcritical mode with 10% spillage, i.e. Agpilage/A, = 0.1 (d) flight dynamic pressure qo
Transcribed Image Text:(a) inlet total pressure recovery with the shock at the lip, i.e. the best backpressure da an obomm (b) inlet total pressure recovery when the shock is inside the duct at A,/A, = 1.2, i.e. the super- critical mode M (@) (C) inlet total pressure recovery in subcritical mode with 10% spillage, i.e. Agpilage/A, = 0.1 (d) flight dynamic pressure qo
6.33 A normal-shock inlet operates in a Mach 1.86 stream with ambient static pressure of Po = Neglecting total pressure loss in the subsonic diffuser, calculate 30 kPa.
Transcribed Image Text:6.33 A normal-shock inlet operates in a Mach 1.86 stream with ambient static pressure of Po = Neglecting total pressure loss in the subsonic diffuser, calculate 30 kPa.
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