Thermodynamic model of a rotating detonation engine

被引：0
作者：
C. A. Nordeen
D. Schwer
F. Schauer
J. Hoke
Th. Barber
B. Cetegen
机构：
[1] University of Connecticut,Mechanical Engineering Department
[2] Naval Research Laboratory Center for Reactive Flow and Dynamical Systems,undefined
[3] Air Force Research Laboratory Propulsion Directorate,undefined
[4] Innovative Scientific Solutions Inc.,undefined
来源：
Combustion, Explosion, and Shock Waves | 2014年 / 50卷
关键词：
rotating detonation engine; continuous detonation; thermodynamic model; ZND model; velocity triangles; Euler turbine equation; swirl;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
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.
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页码：568 / 577
页数：9
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