Multiaxis thrust-vectoring nozzles can furnish substantial combat performance gains for military aircraft; in pursuit of these gains, NASA-Langley has conducted an extensive experimental research program encompassing both static and freestream performance evaluations for numerous multiaxis thrust-vectoring nozzle concepts using air-powered simulation models. An evaluation is presently made of a selection of these experimental results. Two-dimensional and axisymmetric convergent-divergent configurations and hybrid configurations, with and without postexit vanes, have been studied.
Results from NASA Langley experimental studies of multiaxis thrust vectoring nozzles
01.10.1988
Aufsatz (Konferenz)
Keine Angabe
Englisch
Results from NASA Langley Experimental Studies of Multiaxis Thrust Vectoring Nozzles
SAE Technical Papers | 1988
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