Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.

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Bibliographic Details
Main Author: Wing, David J.
Corporate Author: Langley Research Center
Format: Government Document Microfilm 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:

MARC

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245 1 0 |a Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle  |h [microform] /  |c David J. Wing. 
260 |a Hampton, Va. :  |b National Aeronautics and Space Administration, Langley Research Center ;  |a [Springfield, Va.] :  |b [National Technical Information Service, distributor],  |c [1994] 
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650 7 |a Coanda effect.  |2 nasat. 
650 7 |a Computational fluid dynamics.  |2 nasat. 
650 7 |a Convergent-divergent nozzles.  |2 nasat. 
650 7 |a Flow visualization.  |2 nasat. 
650 7 |a Fluidics.  |2 nasat. 
650 7 |a Secondary flow.  |2 nasat. 
650 7 |a Static tests.  |2 nasat. 
650 7 |a Thrust vector control.  |2 nasat. 
650 7 |a Two dimensional models.  |2 nasat. 
650 7 |a Two fluid models.  |2 nasat. 
650 7 |a Wind tunnel tests.  |2 nasat. 
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