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Performance of a 10 deg conical plug nozzle with a stowed thrust reverser at Mach numbers from 0 to 2.0Low angle conical plug nozzle with stowed thrust reverser performance at Mach 0 to 2.0
Document ID
19700033121
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Steffen, F. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-2116
Report Number: NASA-TM-X-2116
Accession Number
70N42437
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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