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Validation of WIND for a Series of Inlet FlowsValidation assessments compare WIND CFD simulations to experimental data for a series of inlet flows ranging in Mach number from low subsonic to hypersonic. The validation procedures follow the guidelines of the AIAA. The WIND code performs well in matching the available experimental data. The assessments demonstrate the use of WIND and provide confidence in its use for the analysis of aircraft inlets.
Document ID
20020092095
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Slater, John W. (NASA Glenn Research Center Cleveland, OH United States)
Abbott, John M. (NASA Glenn Research Center Cleveland, OH United States)
Cavicchi, Richard H. (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2002
Subject Category
Aerodynamics
Report/Patent Number
E-13597
NASA/TM-2002-211907
NAS 1.15:211907
AIAA Paper 2002-0669
Meeting Information
Meeting: 40th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 14, 2002
End Date: January 17, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 708-90-43
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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