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FORTRAN program for calculating velocities in a magnified region on a blade to blade stream surface of a turbomachineFORTRAN computer program for detailed solution of compressible, subsonic, nonviscous flow at leading or trailing edges of blade surface
Document ID
19690013573
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Katsanis, T. (NASA Lewis Research Center Cleveland, OH, United States)
Mc Nally, W. D. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5091
Accession Number
69N22938
Funding Number(s)
CONTRACT_GRANT: 126-15-02-31-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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