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Author

Plentovich, Elizabeth B.

Title Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds [electronic resource] / E.B. Plentovich, Julio Chu, and M.B. Tracy.

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.

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Connect to https://permanent.fdlp.gov/lps67795/19910017810.pdf

Copies

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.60:3099	---	Available

Description	51 p. : ill. ; 28 cm.
Series	NASA technical paper ; 3099
Note	"July 1991"--Cover.
Form	Mode of access: Internet via the NTRS web site.
Bibliography	Includes bibliographical references (p. 5-6).
Subject	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.
Added Author	Chu, Julio.
	Tracy, Maureen B.
	United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Gpo Item No.	0830-H-15 (online)
Sudoc No.	NAS 1.60:3099