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Numerical study of control of dynamic properties of a supersonic inlet using bypass bleedNumerical study on controlling dynamic properties of supersonic inlet using bypass bleed
Document ID
19710005194
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Matthews, C. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-6144
L-7296
Report Number: NASA-TN-D-6144
Report Number: L-7296
Accession Number
71N14669
Funding Number(s)
CONTRACT_GRANT: 720-03-10-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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