NASA NTRS · 19670048102
Inlet flowfield analysis for high Mach number applications.
Abstract
Flow fields of inlets for real or perfect gases determined through four methods for application to supersonic and hypersonic flight regimes
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Benefield, J. W., Hair, L. M.. 1967-05-01. Inlet flowfield analysis for high Mach number applications.. https://ntrs.nasa.gov/citations/19670048102
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