Cover Image

Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

Bibliographic Details
Main Authors: Berrier, Bobby L. (Author), Re, Richard J. (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 ; 1766.
Subjects:
Convergent-divergent nozzles.
Mach number.
Nozzle design.
Performance tests.
Pressure ratio.
Online Access:https://purl.fdlp.gov/GPO/gpo71372
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 (215 pages) : chiefly illustrations.
Bibliography:Includes bibliographical references (page 23).