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Transonic flow studiesMajor emphasis was on the design of shock free airfoils with applications to general aviation. Unsteady flow, transonic flow, and shock wave formation were examined.
Document ID
19810009506
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Seebass, A. R. (Arizona Univ. Tucson, AZ, United States)
Fung, K. Y. (Arizona Univ. Tucson, AZ, United States)
Date Acquired
September 4, 2013
Publication Date
February 28, 1981
Subject Category
Aerodynamics
Report/Patent Number
TFD-81-01
NASA-CR-163965
Report Number: TFD-81-01
Report Number: NASA-CR-163965
Accession Number
81N18029
Funding Number(s)
CONTRACT_GRANT: NSG-2112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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