Thrust Nozzle Design Study for a Quasi-Axisymmetric Scramjet-Powered Vehicle

Title
Thrust Nozzle Design Study for a Quasi-Axisymmetric Scramjet-Powered Vehicle
Authors
Keywords
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Journal
JOURNAL OF PROPULSION AND POWER
Volume 27, Issue 1, Pages 40-49
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2010-12-28
DOI
10.2514/1.48586

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