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Experimental investigation of dynamic distortion in a Mach 2.50 inlet with 60 percent internal contraction and its effect on turbojet stall marginDynamic distortion of supersonic wind tunnel for turbojet engines
Document ID
19690029214
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Calogeras, J. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1842
E-5102
Report Number: NASA-TM-X-1842
Report Number: E-5102
Accession Number
69N38599
Funding Number(s)
CONTRACT_GRANT: 126-15-02-11-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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