Development of a Three-dimensional Transient Wall Heat Transfer Model of a Rotating Detonation Combustor
Author:
Affiliation:
1. National Energy Technology Laboratory
2. West Virginia University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0902
Reference9 articles.
1. Research on Pulse Detonation Combustion Systems: A Status Report
2. Detonative propulsion
3. Heat fluxes to combustor walls during continuous spin detonation of fuel-air mixtures
4. Theuerkauf, S. W. "Heat Exchanger Design and Testing for a 6-inch Rotating Detonation Engine", MS Thesis, AFIT-ENY-13-M-33,Air Force Institute of Technology, WP AFB, Ohio,2013.
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