Time-Accurate Flow Field and Rotor Speed Measurements of a Pulsed Detonation Driven Turbine
Author:
Affiliation:
1. Air Force Institute of Technology
2. Air Force Research Laboratory
3. Innovative Scientific Solutions, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-577
Reference12 articles.
1. 1Dyer, R.S., and Kaemming, T.A. "The Thermodynamic Basis of Pulsed Detonation Engine Thrust Production," AIAA 2002-4072,38th AIAA/ASME/SAE/ASEE JointPropulsion Conference, July2002.
2. Integration of a pulsed detonation engine with an ejector pump and with a turbo-charger as methods to self-aspirate
3. 3Rouser, Kurt, King, Paul, Schauer, Fred, Sondergaard, Rolf, and Hoke, John, "Unsteady Performance of a Turbine Driven byaPulseDetonation Engine."AIAA2010-1116,48th AIAAAerospaceSciencesMeeting, Jan 2010.
4. Turbine Efficiency for Unsteady Periodic Flows
5. 5Glaser, Aaron, Caldwell, Nicholas, Gutmark, Ephraim, "Performance of an Axial Flow Turbine Driven by Multiple Pulse Detonation Combustors."AIAA2007-1244,45th AIAAAerospaceSciencesMeeting, Jan 2007.
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