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Preliminary transonic performance results for solid and slotted turbojet nacelle afterbodies incorporating fixed divergent jet nozzles designed for supersonic operationTransonic performance of three turbojet nozzle- afterbody configurations
Document ID
19650003123
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Runckel, J. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1958
Subject Category
Aerodynamics
Report/Patent Number
NASA-MEMO-10-24-58L
Report Number: NASA-MEMO-10-24-58L
Accession Number
65N12724
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
JET NOZZLE
AFTERBODY
TURBOJET ENGINE

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