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
Description
Item Description:"February 1985."
Physical Description:1 online resource (66 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 7-8).

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