Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Bibliographic Details
Main Author: Kapoor, Kamlesh
Corporate Author: United States National Aeronautics and Space Administration
Other Authors: Anderson, Bernhard H, Shaw, Robert J (Robert Joseph), 1946-
Format: Government Document Book
Language:English
Published: [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1994]
Series:NASA technical memorandum 106580
Subjects:
Computational fluid dynamics
Corner flow
Hypersonic inlets
Hypersonic speed
Inlet flow
Shock wave interaction
Supersonic speed
Turbulent boundary layer
Two dimensional flow

Internet

Stanford University

Holdings details from Stanford University
Call Number: NAS 1.15:106580

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