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Airfoil characteristics in a nonequilibrium ambient stream based on linearized theoryAerodynamic characteristics of thin airfoil in nonequilibrium stream at small angle of attack
Document ID
19640011348
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Der, J. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1964
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TR-R-201
Report Number: NASA-TR-R-201
Accession Number
64N21262
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THIN AIRFOIL
NONEQUILIBRIUM FLOW
AERODYNAMIC CHARACTERISTICS

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