NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Investigation of Translating-spike Supersonic Inlet as Means of Mass-flow Control at Mach Numbers of 1.5, 1.8, and 2.0
Document ID
19930087622
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gorton, Gerald C
Date Acquired
August 16, 2013
Publication Date
October 29, 1953
Report/Patent Number
NACA-RM-E53G10
Report Number: NACA-RM-E53G10
Accession Number
93R16912
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available