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Inlet flowfield analysis for high Mach number applications.Flow fields of inlets for real or perfect gases determined through four methods for application to supersonic and hypersonic flight regimes
Document ID
19670048102
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Benefield, J. W.
Hair, L. M.
Date Acquired
August 3, 2013
Publication Date
May 1, 1967
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 66-605
Report Number: AIAA PAPER 66-605
Accession Number
67A26831
Funding Number(s)
CONTRACT_GRANT: NAS8-20082
Distribution Limits
Public
Copyright
Other
Keywords
REAL GAS
HYPERSONIC FLIGHT
FLOW FIELD
INLET FLOW

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