Rotating Detonation Rocket Engine Operability Under Varied Pressure Drop Injection

Title
Rotating Detonation Rocket Engine Operability Under Varied Pressure Drop Injection
Authors
Keywords
-
Journal
JOURNAL OF SPACECRAFT AND ROCKETS
Volume -, Issue -, Pages 1-10
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2020-09-12
DOI
10.2514/1.a34763

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