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A Numerical Study of Hypersonic Forebody/Inlet Integration ProblemA numerical study of hypersonic forebody/inlet integration problem is presented in the form of the view-graphs. The following topics are covered: physical/chemical modeling; solution procedure; flow conditions; mass flow rate at inlet face; heating and skin friction loads; 3-D forebogy/inlet integration model; and sensitivity studies.
Document ID
19910016029
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Kumar, Ajay (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
January 10, 1991
Publication Information
Publication: Computational Fluid Dynamics Code Validation(Calibration. JANNAF Airbreathing Propulsion Subcommittee Workshop: High-Speed Inlet Forebody Interactions
Subject Category
Aerodynamics
Meeting Information
Meeting: JANNAF Workshop on CFD Code Validation/Calibration for High-Speed Inlet Forebody Interactions
Location: Reno, NV
Country: United States
Start Date: January 10, 1991
End Date: January 11, 1991
Sponsors: Department of the Navy, NASA Headquarters, Department of the Air Force, Department of the Army
Accession Number
91N25343
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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