Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities /

Bibliographic Details

Main Author:	Leavitt, Laurence D.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Other Authors:	Burley, James R.
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Series:	NASA technical paper ; 2519.
Subjects:	Nozzle geometry. Static tests. Thrust reversal. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/LPS122510