Pressure Gain Combustor Component Viability Assessment Based on Initial Testing
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Publisher
American Institute of Aeronautics and Astronautics
Reference7 articles.
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3. Matsutomi, Y., Hein, C., Lian, C., Meyer, S., Merkle, C. and Heister, S. "Facility Development for Testing of Wave Rotor Combustion Rig," AIAA-2007-5052, 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, July8-11,2007Source of ignition flow: Withdrawal of gas flow preceding passage P source > P torch Currently 1.8% of total mass flow
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