NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Performance of a mach 3.0 external-internal- compression axisymmetric inlet at mach numbers from 2.0 to 3.5External-internal-compression axisymmetric inlet performance at supersonic speeds
Document ID
19650003099
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Salmi, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Stitt, L. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-145
Accession Number
65N12700
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INTERNAL COMPRESSION INLET
AXISYMMETRY
SUPERSONIC SPEED

Related Records

There are no records associated with this record.
No Preview Available