Design of an Optically-Accessible Rotating Detonation Engine
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference8 articles.
1. 3Schwer, D.A., and Kailasanth, K. "Effect of Inlet on Fill Region and Performance of Rotating Detonation Engines," AIAA Paper 2011-6044, 47thAIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Diego, CA, 31July- 03 August2011.
2. Continuous spin detonation of fuel-air mixtures
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