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An Experimental Investigation of Circular Internal-Compression Inlets with Translating Centerbodies Employing Boundary-Layer Removal at Mach Numbers from 0.85 to 3.50Effect of boundary layer removal on total pressure recovery - circular internal compression inlets with translating centerbodies
Document ID
19630004007
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Pfyl, F. A. (NASA Ames Research Center Moffett Field, CA, United States)
Watson, E. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-MEMO-2-19-59A
Accession Number
63N13883
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INTERNAL COMPRESSION INLET
BOUNDARY LAYER CONTROL
PRESSURE RECOVERY

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