Unsteady Performance of Rotating Detonation Engines with Different Exhaust Nozzles

标题
Unsteady Performance of Rotating Detonation Engines with Different Exhaust Nozzles
作者
关键词
-
出版物
JOURNAL OF PROPULSION AND POWER
Volume 33, Issue 1, Pages 121-130
出版商
American Institute of Aeronautics and Astronautics (AIAA)
发表日期
2016-11-14
DOI
10.2514/1.b36164

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