Cover Image

Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed /

Bibliographic Details
Main Author: Jones, Daniel S. (Author)
Format: Government Document eBook
Language:English
Published: Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, October 2014.
Series:NASA technical memorandum ; 2014-218376.
Subjects:
Convergent-divergent nozzles.
Flow distribution.
Inviscid flow.
Nozzle design.
Rocket nozzles.
Online Access:https://purl.fdlp.gov/GPO/gpo58350
http://purl.fdlp.gov/GPO/gpo58350
Description
Item Description:Title from title screen (viewed July 2, 2015).
"October 2014."
Physical Description:1 online resource (25 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 14).