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Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversingThe effects of geometric design parameters on the internal performance of nonaxisymmetric single expansion-ramp nozzles were investigated at nozzle pressure ratios up to approximately 10. Forward-flight (cruise), vectored-thrust, and reversed-thrust nozzle operating modes were investigated.
Document ID
19820012282
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Re, R. J. (NASA Langley Research Center Hampton, VA, United States)
Berrier, B. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
NASA-TP-1962
NAS 1.60:1962
L-14902
Report Number: NASA-TP-1962
Report Number: NAS 1.60:1962
Report Number: L-14902
Accession Number
82N20156
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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