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