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Wind tunnel investigation of techniques for reducing cowl drag of an axisymmetric external-compression inlet at Mach 2.49

J. E. Calogeras, E. T. Meleason

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Abstract

Wind tunnel investigation of techniques for reducing cowl drag of external compression inlet at Mach 2.49

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Wind tunnel investigation of techniques for reducing cowl drag of external compression inlet at Mach 2.49

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OpenAlex reports 4 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Wind tunnel investigation of techniques for reducing cowl drag of external compression inlet at Mach 2.49

Key concepts: Drag, Drag divergence Mach number, Mach number, Inlet, Wave drag, Wind tunnel, Mechanics, Compression (physics)

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Wind tunnel investigation of techniques for reducing cowl drag of an axisymmetric external-compression inlet at Mach 2.49 — Research Paper | ScholarLens