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This article is cited in 70 scientific papers (total in 70 papers)
Thermodynamic model of a rotating detonation engine
C. A. Nordeena, D. Schwerb, F. Schauerc, J. Hoked, T. Barbera, B. Cetegena a Mechanical Engineering Department, University of Connecticut, Storrs, CT, 06269-3139, USA
b Naval Research Laboratory Center for Reactive Flow and Dynamical Systems, Code 6410, Washington, DC, 20375, USA
c Air Force Research Laboratory Propulsion Directorate, Wright-Patterson AFB, OH, 45433, USA
d Innovative Scientific Solutions Inc., Dayton, OH, USA
Abstract:
The conventional Zel'dovich–von Neumann–Döring (ZND) detonation theory is modified with two-dimensional velocity vectors to account for the performance and steady-state flow features of a rotating detonation engine. The developed analytical model explains many of the steady-state features of the rotating detonation and its thermodynamics. The generation of swirl is shown to be the primary mechanism of energy transfer.
Keywords:
rotating detonation engine, continuous detonation, thermodynamic model, ZND model, velocity triangles, Euler turbine equation, swirl.
Received: 05.04.2013 Revised: 07.10.2013
Citation:
C. A. Nordeen, D. Schwer, F. Schauer, J. Hoke, T. Barber, B. Cetegen, “Thermodynamic model of a rotating detonation engine”, Fizika Goreniya i Vzryva, 50:5 (2014), 75–86; Combustion, Explosion and Shock Waves, 50:5 (2014), 568–577
Linking options:
https://www.mathnet.ru/eng/fgv172 https://www.mathnet.ru/eng/fgv/v50/i5/p75
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