Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions

Published 2013 View Full Article

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Title
Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions
Authors
Keywords
Scramjet, Optimization, Nozzle
Journal
SHOCK WAVES
Volume 23, Issue 5, Pages 453-460
Publisher
Springer Nature
Online
2013-05-20
DOI
10.1007/s00193-013-0449-4
References
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