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Characteristics study of a bicone mixed-compression inlet for Mach 1.80 to 2.50
Espandi opera
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Design of supersonic inlets by a computer program incorporating the method of characteristics
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Design-of-experiments to reduce life-cycle costs in combat aircraft inlets
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Experimental investigation of the application of microramp flow control to an oblique shock interaction
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Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets
Espandi opera
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