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 Development and Validation of a
Massively Parallel Flow Solver for Turbomachinery Flows, AIAA Paper 00-0882, Reno, Jan. 2000
 Computation of Flow in a Compressor
Blade Row by a Third-Order AccurateScheme, AIAA Paper 98-3561, Cleveland, Jul. 1998
 Computation of Steady Flow in a Turbomachinery Stage by a Third-Order Accurate
High-Resolution Scheme, AIAA Paper 98-0920, Reno, Jan. 1998
 "The Numerical Simulation of Multistage Transonic Compressor Steady/Unsteady Flows by Third Order Accurate UNO Scheme", 3rd International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows (ISAIF), Beijing, 1996
 "The Organizing and Controlling of Three-Dimensional Shock in Modern Transonic Compressor Rotors", International Symposium of Fluid Machinery and Fluid Engineering, Beijing, 1996
 "The High- Resolution schemes and Numerical Simulation of Complex Flow in Turbomachinery Blade Row", 1995 YOKOHAMA International Gas Turbine Congress.
 "The High Resolution Numerical Simulation of 3D Compressible Viscous Flows in Turbomachinery", 6th International Symposium on Computational Fluid Dynamics", Sep. 1995,Nevada,USA.
 "The Implicit High-Resolution Numerical Analysis of Three Dimensional Turbulence Flows in Compressor Blade Rows", J. of Aeroapse Power, 1996
 "An Implicit High-Resolution Solver for Flows around Cascades", J. of Aeroapse Power (in Chinese), Vol.10, No.2, 1995
 "A High-Resolution Scheme for Numerical Simulation of Shocked Flow and It's Application", Proceedings of Third China-Russia-Ukraine Symposium on Astronautical Science and Technology. Xian, Oct.,1994, pp 420-423, ISBN 7-5612-0672-O/V.18
 "The Numerical Simulation of Spanwise Mixing in Multistage Compressors", J. of Aerospace Power, Vol.9, No.1,1994
Last Modified: January, 2000