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
Abstract
J. E. Calogeras, E. T. Meleason
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
Key concepts: Drag, Drag divergence Mach number, Mach number, Inlet, Wave drag, Wind tunnel, Mechanics, Compression (physics)