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
1988-10-01
Conference paper
No indication
English
Results from NASA Langley Experimental Studies of Multiaxis Thrust Vectoring Nozzles
SAE Technical Papers | 1988
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