Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle

Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle

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Bibliographic Details
Main Author: Wing, David J
Corporate Author: Langley Research Center
Format: Government Document Book
Language:English
Published: Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1994]
Series:NASA technical memorandum 4574
Subjects:
Coanda effect
Computational fluid dynamics
Convergent-divergent nozzles
Flow deflection
Flow visualization
Fluidics
Jet thrust
Nozzle flow
Secondary flow
Static tests
Thrust vector control
Two dimensional flow
Two dimensional models
Two fluid models
Wind tunnel tests
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Stanford University

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Call Number: NAS 1.15:4574

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