Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability /

Bibliographic Details
Main Author:	Bangert, Linda S.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors:	Leavitt, Laurence D.
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Series:	NASA technical paper ; 2933.
Subjects:	Jet planes > Thrust reversers > Testing. Deflectors. Flow deflection. Static tests. Thrust reversal. Thrust vector control. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/LPS60139

Available Online