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Flight investigation of installation effects on a plug nozzle installed on an underwing nacelleFlight test investigation of effects of variable geometry plug nozzles installed on f-106b aircraft
Document ID
19710020807
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chamberlin, R. (NASA Lewis Research Center Cleveland, OH, United States)
Samanich, N. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
E-5546
NASA-TM-X-2295
Report Number: E-5546
Report Number: NASA-TM-X-2295
Accession Number
71N30283
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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