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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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BibTeXRIS

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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