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PERFORMANCE OF A MACH NUMBER 3.0 DESIGN AXISYMMETRIC DOUBLE-CONE EXTERNAL-COMPRESSION INLET IN THE MACH NUMBER RANGE 1.97 TO 0.79Axisymmetric double cone external compression inlet in transonic range - drag components at detached shock conditions
Document ID
19630006260
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
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-154
Accession Number
63N16136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK WAVE
AIR INLET
DRAG MEASUREMENT
TRANSONIC SPEED
CONICAL INLET

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