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AN EXPERIMENTAL INVESTIGATION AT MACH NUMBERS FROM 2.1 TO 3.0 OF CIRCULAR INTERNAL-COMPRESSION INLETS HAVING TRANSLATABLE CENTERBODIES AND PROVISIONS FOR BOUNDARY-LAYER REMOVALInlets having translatable centerbodies and provision for boundary layer removal
Document ID
19630004019
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Watson, E. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1960
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-156
Report Number: NASA-TM-X-156
Accession Number
63N13895
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR INLET
BOUNDARY LAYER CONTROL

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