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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

Internet

https://purl.fdlp.gov/GPO/LPS67795

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Call Number: NAS 1.60:3099
 
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Call Number: NAS 1.60:3099
 
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