Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
By: E.B. Plentovich, Julio Chu, and M.B. Tracy.
Contributors: Chu, Julio.; Tracy, M. B.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA technical paper -- 3099.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; For sale by the National Technical Information Service]
Published: 1991
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 51
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.
Notes: "July 1991"--Cover.

Includes bibliographical references (p. 5-6).

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1991. 1 microfiche : negative.