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PERFORMANCE SUMMARY AND ANALYSIS OF A MACH 3.0 DESIGN AXISYMMETRIC ALL-EXTERNAL-COMPRESSION DOUBLE-CONE INLET FROM MACH NUMBER 3.0 TO 0.8Axisymmetric external compression double cone inlet - mach 3 to 0.8 - pressure recovery, mass flow ratio, cowl pressure and additive drag
Document ID
19630006259
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Allen, J. L. (NASA Lewis Research Center Cleveland, OH, United States)
Davis, O. H. (NASA Lewis Research Center Cleveland, OH, United States)
Mitchell, G. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1960
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-149
Report Number: NASA-TM-X-149
Accession Number
63N16135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR INLET
MASS FLOW
DRAG
COMPRESSION
COWLING
PRESSURE RECOVERY
AXISYMMETRY
CONICAL INLET

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