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

Bibliographic Details
Main Author:	Plentovich, Elizabeth B.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Other Authors:	Chu, Julio, Tracy, M. B.
Format:	Government Document Microform Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; 1991.
Series:	NASA technical paper ; 3099.
Subjects:	Aerodynamic load. Aerodynamics, Transonic. Cavities (Airplanes) Reynolds number. Turbulent boundary layer. Yawing (Aerodynamics) Cavities. Flow distribution. High Reynolds number. Mach number. Pressure distribution. Subsonic flow. Transonic flow. Yaw.
Online Access:	https://purl.fdlp.gov/GPO/LPS67795

Description
Item Description:	"July 1991"--Cover. Microform.
Physical Description:	51 pages : illustrations ; 28 cm. Also 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.
Bibliography:	Includes bibliographical references (pages 5-6).