Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° /

Bibliographic Details
Main Authors:	Berrier, Bobby L. (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, October 1984.
Series:	NASA technical paper ; 2364.
Subjects:	Axisymmetric bodies. Nozzle thrust coefficients. Static tests. Thrust vector control. Transonic wind tunnels. Two dimensional flow.
Online Access:	https://purl.fdlp.gov/GPO/gpo76455

Description
Item Description:	"October 1984"--Report documentation page. "Performing organization: NASA Langley Research Center"--Report documentation page.
Physical Description:	1 online resource (141 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 11).