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Study of design and analysis methods for transonic flowAn airfoil design program and a boundary layer analysis were developed. Boundary conditions were derived for ventilated transonic wind tunnels and performing transonic windtunnel wall calculations. A computational procedure for rotational transonic flow in engine inlet throats was formulated. Results and conclusions are summarized.
Document ID
19770023142
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Murman, E. M. (Flow Research, Inc. Kent, WA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1977
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-152041
NOTE-118
Report Number: NASA-CR-152041
Report Number: NOTE-118
Accession Number
77N30086
Funding Number(s)
CONTRACT_GRANT: NAS2-8847
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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