Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct

Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct

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Bibliographic Details
Main Authors:	Wing, David J, Wing, David J (David John)
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, [1998]
Series:	NASA technical paper 206912 NASA technical paper 206912
Subjects:	Angular distribution Convergent nozzles Flapping Flow distribution Nozzle geometry Pitch (Inclination) Thrust vector control
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Stanford University

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Call Number:	ISIL:US-CST NAS 1.60:206912