Influence of Unsteadiness on the Analysis of Pressure Gain Combustion Devices
Author:
Affiliation:
1. Controls and Dynamics Branch, NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44130
2. Innovative Scientific Solutions, Inc., Dayton, Ohio 45440
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34913
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1. Detonation Initiation Studies and Performance Results for Pulsed Detonation Engine Applications
2. Thermodynamic Cycle Analysis of Pulse Detonation Engines
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4. Thermodynamics of Airbreathing Pulse-Detonation Engines
5. Constant Volume Limit of Pulsed Propulsion for a Constant ? Ideal Gas
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