Research on supersonic inlet bleed /

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Bibliographic Details
Author / Creator:Davis, David O.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Description:1 online resource (24 p.) : ill. (some col.).
Series:NASA/TM ; 2012-217620
NASA technical memorandum ; 2012-217620.
Subject:Flow coefficients.
Supersonic inlets.
Boundary layers.
Computational fluid dynamics.
Free flow.
Mach number.
Reynolds number.
Computational fluid dynamics.
Mach number.
Reynolds number.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:
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Other authors / contributors:Vyas, Manan A.
Slater, John W.
NASA Glenn Research Center.
AIAA Aerospace Sciences Meeting (50th : 2012 : Nashville, Tenn.)
Notes:Title from title screen (viewed on Dec. 10, 2012).
"August 2012."
"Prepared for the 50th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Nashville, Tennessee, January 9-12, 2012."
Includes bibliographical references (p. 24).
Sponsored by National Aeronautics and Space Administration WBS 984754.
GPO item no.:0830-D (online) classification:NAS 1.15:2012-217620