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

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:	https://purl.fdlp.gov/GPO/gpo107941