Quantification of the Loss Mechanisms of a Ram Rotating Detonation Engine-Reference-Cited by-同舟云学术

Quantification of the Loss Mechanisms of a Ram Rotating Detonation Engine

Published:2020-01-05 Issue: Volume: Page:
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Container-title:AIAA Scitech 2020 Forum
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Author:

Kaemming Thomas A.¹,Fotia Matthew L.¹,Hoke John¹,Schumaker Stephen A.²,Schauer Frederick R.³

Affiliation:

1. Innovative Scientific Solutions, Inc.

2. Air Force Research Laboratory

3. Air Force Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. Power, Vol. 18, No. 1, 2002, pp. 68-76 [2] Dyer, R.S. and Kaemming, T.A. "The Thermodynamic Basis of a Pulse Detonation Engine Thrust Production," AIAA 2002-

2. 4072, 2002. [3] Paxson, D.E. and Kaemming, T.A. "Influence of Unsteadiness on the Analysis of Pressure Gain Combustion Devices,"

3. Through a Reduced-Order Approach," Journal of Propulsion and Powervolume33, issue 1,2017, pp131to 143 doi: 10.2514/1.b36237

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