Research on supersonic inlet bleed /

Saved in:

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.).
Language:	English
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:	http://pi.lib.uchicago.edu/1001/cat/bib/8951488

Hidden Bibliographic Details
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." "AIAA-2012-0272." Includes bibliographical references (p. 24). Sponsored by National Aeronautics and Space Administration WBS 984754.02.07.03.13.02 E-18208
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:2012-217620

Similar Items