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David J. Wing has written:

'Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability' -- subject(s): Static models, Transonic wind tunnels, Thrust vector control, Nozzle flow, Internal flow, Convergent-divergent nozzles, Contours

'Performance characteristics of two multiaxis thrust-vectoring nozzles at Mach numbers up to 1.28' -- subject(s): Nozzles

'Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle' -- subject(s): Computational fluid dynamics, Thrust vector control, Coanda effect, Wind tunnel tests, Fluidics, Static tests, Flow visualization, Secondary flow, Two dimensional models, Two fluid models, Convergent-divergent nozzles

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10y ago

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