NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle conceptsEffects of several geometric parameters on the internal performance of nonaxisymmetric convergent-divergent, single-ramp expansion, and wedge nozzles were investigated at nozzle pressure ratios up to approximately 10. In addition, two different thrust-vectoring schemes were investigated with the wedge nozzle. The results indicated that as with conventional round nozzles, peak nonaxisymmetric nozzle, internal performance occurred near the nozzle pressure ratio required for fully expanded exhaust flow. Nozzle sidewall length or area generally had little effect on the internal performance of the nozzles investigated.
Document ID
19790017851
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Berrier, B. L. (NASA Langley Research Center Hampton, VA, United States)
Re, R. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-TP-1468
L-12810
Accession Number
79N26022
Funding Number(s)
PROJECT: RTOP 505-04-13-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available