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Inverse transonic airfoil design methods including boundary layer and viscous interaction effectsThe development and incorporation into TRANDES of a fully conservative analysis method utilizing the artificial compressibility approach is described. The method allows for lifting cases and finite thickness airfoils and utilizes a stretched coordinate system. Wave drag and massive separation studies are also discussed.
Document ID
19790009634
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Carlson, L. A. (Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 3, 2013
Publication Date
January 31, 1979
Subject Category
Aerodynamics
Report/Patent Number
TAMRF-3224-79-01
NASA-CR-158136
Report Number: TAMRF-3224-79-01
Report Number: NASA-CR-158136
Accession Number
79N17805
Funding Number(s)
CONTRACT_GRANT: NSG-1174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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