Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/

Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/

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Bibliographic Details
Main Author:	Leavitt, Laurence D. (Author)
Corporate Author:	Langley Research Center.
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, February 1985.
Series:	NASA technical paper ; 2391.
Subjects:	Convergent. Thrust vector control. Wind tunnel tests. Nozzle flow. Transonic wind tunnels.
Online Access:	CONNECT CONNECT

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