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Effect of porous bleed in a high performance axisymmetric, mixed compression inlet at Mach 2.50Effects of boundary layer bleed rate and location on performance of axisymmetric inlet designed for Mach 2.5
Document ID
19690000963
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cubbison, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Johnson, D. F. (NASA Lewis Research Center Cleveland, OH, United States)
Meleason, E. T. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1692
Report Number: NASA-TM-X-1692
Accession Number
69N10294
Funding Number(s)
CONTRACT_GRANT: 126-15-02-11-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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