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M. Cooper, S. Jackson, J. Austin, E. Wintenberger, J. Shepherd (2001)
Direct Experimental Impulse Measurements for Detonations and DeflagrationsJournal of Propulsion and Power, 18
Jackson Cooper (2001)
Direct Experimental Impulse Measurements for Detonations and Deflagrations. AIAA 2001–3812
Z. Zhang, S. Yu, Hao He, P. Jorgenson (2001)
Direct Calculations of Plume Dynamics of a Pulse Detonation Engine by the CE/SE Method
Z. Zhang, S. Yu, Xiao-Yen Wang, Sin-Chung Chang, A. Himansu, P. Jorgenson (2000)
The CE/SE Method for Navier-Stokes Equations Using Unstructured Meshes for Flows at All Speeds
Masayoshi Shimo, S. Meyer, S. Heister, C. Weng, Jun Ji, J. Gore (2002)
An Experimental and Computational Study of Pulsed Detonations in a Single Tube
H. Ebrahimi, R. Mohanraj, C. Merkle (2001)
Modeling of Multi-Tube Pulse Detonation Engine Operation
Z. Zhang, S. Yu (2001)
A Generalized Space-Time CE/SE Method for the Euler Equations on Quadrilateral and Hexagonal Meshes
S.T. Yu
Treatments of Stiff Source Terms in Conservation Laws by the method of Space-Time Conservation Element and Solution Element. AIAA-97–0435
Z.C. et al. Zhang (2000)
The CE/SE method for Naver-Stokes Equations Using Unstructured Meshes for Flows at all Speeds. AIAA-2000–0393
S. Yu, Sin-Chung Chang (1997)
Treatments of stiff source terms in conservation laws by the method of space-time conservation element/solution element
K. Kailasanath (2001)
Computational Studied of Pulse Detonation Engines. In: Proceedings of the 14th ONR Propulsion MeetingProceedings of the 14th ONR Propulsion Meeting
Z.C. Zhang (2001)
Direct Calculations of Plume Dynamics of a Pulse Detonation Engine by the Space-Time CE/SE method. AIAA-2001–3614
Sin-Chung Chang (1995)
The Method of Space-Time Conservation Element and Solution Element-A New Approach for Solving the Navier-Stokes and Euler EquationsJournal of Computational Physics, 119
H.B. Ebrahimi (2001)
Modeling of Multi-tube pulse Detonation Engine Operation. In: Proceedings of 14th ONR Propulsion MeetingProceedings of 14th ONR Propulsion Meeting
S.T. et al. Yu (2001)
A Numerical Study of Detonation Dynamics in a JP10 Fueled PDE by the CE/SE method. In: Proceedings of 14th ONR Propulsion MeetingProceedings of 14th ONR Propulsion Meeting
Z.C. Zhang (2001)
A Generalized Space-Time CE/SE method for the Euler Equations on Quadrilateral and Hexagonal Meshes. AIAA-2001–2592
M. Shimo (2002)
An experimental and Computational Study of Pulse Detonation in a Single Tune. In: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Abstract. In this paper, the CE/SE method is developed to simulate the two- and three-dimensional flow-field of Pulse Detonation Engine (PDE). The conservation equations with stiff source terms for chemical reaction are solved in two steps. The detailed analysis of computational results of a PDE with a single detonation tube and a PDE with five detonation tubes are given in this paper. Complex wave systems are observed inside and outside a PDE. For a PDE with 5 detonation tubes, there is a big bow shock produced from a number of little shocks near the open ends of tubes. A lot of vortexes interact with shocks and a large expansion wave propagates forward and backward with respect to the PDE in a semi-oval shape.
"Acta Mechanica Sinica" – Springer Journals
Published: Feb 1, 2005
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