Average and Instantaneous Heat Release to the Walls of an RDE
Author:
Affiliation:
1. Air Force Research Laboratory
2. Innovative Scientific Solutions, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-1503
Reference5 articles.
1. Heat fluxes to combustor walls during continuous spin detonation of fuel-air mixtures
2. Theuerkauf, Scott W. Heat Exchanger Design and Testing for a 6-Inch Rotating Detonation Engine. MS Thesis, AFIT-ENY-13-M-33. Graduate School of Engineering and Management,Air Force Institute of Technology (AU). Wright-Patterson AFB OH,March 2013.
3. Flowfield Characterization of a Rotating Detonation Engine
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