Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles /

Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles /

Saved in:
Bibliographic Details
Main Authors: Yetter, Jeffery A. (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, December 1980.
Series:NASA technical paper ; 1771.
Subjects:
Convergent-divergent nozzles.
Exhaust flow simulation.
Nozzle design.
Static pressure.
Wind tunnel tests.
Online Access:CONNECT
CONNECT
Description
Item Description:Title from title screen (viewed on Aug. 19, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (116 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 18-19).

Similar Items