- AIAA 99-3277 Copyright American Institute of Aeronautics and Astronautics, Inc., 1999. All rights reserved.
- AIAA 2001-2592 Copyright 2001 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
- SOLVCON: A Python-Based CFD Software Framework for Hybrid Parallelization
- American Institute of Aerospace and Astronautics AIAA-2004-0075
- AIAA-2006-4778 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, California, July 9-12, 2006
- American Institute of Aeronautics and Astronautics Pressure Scaling Effects on Ignition and Detonation
- AIAA JOURNAL Vol. 42, No. 5, May 2004
- American Institute of Aeronautics and Astronautics Simulation of a Supersonic Jet Controlled by Plasma
- Calculations of Low-Mach-Number Viscous Flows without Preconditioning by the Space-Time CE/SE
- AIAA 2000-0393 The CE/SE Method for Navier-Stokes Equations Using
- AIAA JOURNAL Vol. 42, No. 12, December 2004
- AIAA 99-3576 A Non-Oscillatory Central Scheme for Conservation Laws
- Analyses of Direct Detonation Initiation with Realistic Finite-Rate Chemistry
- AIAA 2000-2331 The Space-Time CE/SE Method for the Navier-Stokes
- 1. Research assistant professor, Email: zhangzc@me1.eng.wayne.edu 2. Associate professor, Email: styu@me1.eng.wayne.edu
- Simulation of Cavitating Flows by the Space-Time CE/SE Method Jian-Rong Qin, S.T. John Yu, Zeng-Chan Zhang, Ming-Chia Lai
- Convergence and Error Bound Analysis for the Space-Time CESE Method
- Numerical Calculation of Unstable Detonations by the Method of Space-Time Conservation Element and Solution Element
- CFL Number Insensitive CESE Schemes For the Two-Dimensional Euler Equations
- Application of the CESE Method to Detonation with Realistic Finite-Rate Chemistry
- Application of the CESE Method to PDE Plume Dynamics Using a Beowulf Cluster
- Solving the MHD Equations by the Space-Time Conservation Element and Solution Element Method
- AIAA JOURNAL Vol. 43, No. 10, October 2005
- High-Order CESE Methods for the Euler Equations David L. Bilyeu,
- American Institute of Aeronautics and Astronautics Three-Dimensional Simulations of Cavity Flows
- Direct Calculation of Spherical Detonation Initiation of H2/O2/Ar Mixtures by the CESE Method
- Three-Dimensional Simulation of Transverse Injection in a Supersonic Flow by the CESE Method
- AIAA-2002-3888 Application of the Space-Time Conservation Element and Solution
- Direct Calculation of High-Speed Cavity Flows in a Scramjet Engine by the CESE Method
- AIAA-2001-0531 Direct Calculation of Turbomachinery Flows
- AIAA 2001-0476 Research Associate. AIAA Member, Email: zczhang@me1.eng.wayne.edu
- Simulations of Three-Dimensional Detonations by the CE/SE Method Using a Very Low-Cost Beowulf Cluster
- AIAA 99-0904 Shock Capturing without Riemann Solver
- 1999-01-3554 Direct Calculations of Cavitating Flows in Fuel Delivery
- AIAA-2003-0324 Calculation of the Ideal MHD Equations by the CESE Method
- AIAA 2006-9711, AIAA Sciences Meeting, Reno Nevada American Institute of Aeronautics and Astronautics
- A Unified Wall Boundary Treatment for Viscous and Inviscid Flows in the CE/SE Method
- Direct Calculations of Stable and Unstable ZND Detonations by the Space-Time Conservation Element and Solution Element Method
- Direct Calculations of One-, Two-, and Three-Dimensional Detonations by the CESE Method
- Direct Calculation of Wave Implosion for Detonation Initiation in Pulsed Detonation Engines and S.-T. John Yu
- Journal of Computational Physics 175, 168199 (2002) doi:10.1006/jcph.2001.6934, available online at http://www.idealibrary.com on
- Constructing a Supercomputing Framework by Using Python for Hybrid Parallelism and GPU Cluster
