Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing.

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Bibliographic Details
Online Access: Click here to view paper online
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, [1998]
Series:NASA technical paper ; 206912.
Subjects:

MARC

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245 1 0 |a Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct  |h [microform] /  |c David J. Wing. 
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300 |a 1 volume. 
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533 |a Microfiche.  |b [Washington, D.C. :  |c National Aeronautics and Space Administration,  |d 1998]  |e 2 microfiches. 
650 7 |a Thrust vector control.  |2 nasat. 
650 7 |a Nozzle geometry.  |2 nasat. 
650 7 |a Convergent nozzles.  |2 nasat. 
650 7 |a Angular distribution.  |2 nasat. 
650 7 |a Flow distribution.  |2 nasat. 
650 7 |a Flapping.  |2 nasat. 
650 7 |a Pitch (Inclination)  |2 nasat. 
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