Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds /

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Bibliographic Details
Author / Creator:	Plentovich, Elizabeth B.
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1991.
Description:	51 pages : illustrations ; 28 cm.
Language:	English
Series:	NASA technical paper ; 3099 NASA technical paper ; 3099.
Subject:	Aerodynamic load. Aerodynamics, Transonic. Cavities (Airplanes) Reynolds number. Turbulent boundary layer. Yawing (Aerodynamics)
Format:	E-Resource Microform U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/6505355

Hidden Bibliographic Details
Other authors / contributors:	Chu, Julio. Tracy, M. B. United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Notes:	"July 1991"--Cover. Includes bibliographical references (pages 5-6). Available via Internet from the NTRS web site. Address as of 3/16/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910017810%5F1991017810.pdf; current access is available via PURL.
GPO item no.:	0830-H-15 (MF) 0830-H-15 (online)
Govt.docs classification:	NAS 1.60:3099

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