Shijun Luo, aka Shih-Chun Lo
Researcher
Department of Mechanical and Aerospace Engineering
University of California, Irvine
Irvine, CA 92697-3975
Phone: (949)824-3784          Fax: (949)824-8585
e-mail: sluo@uci.edu          http://luke.eng.uci.edu
Downloadable Resume

EDUCATION:
Ph.D.,  1951,  Magna cum laude, Department of Aeronautics,
  California Institute of Technology, Pasadena, CA
M.S., 1948,  Department of Aeronautical Engineering,
  University of Minnesota, Minneapolis, MN
B.S., 1945,  Department of Aeronautical Engineering,
  National Central University, Chongqing, China

AREA OF SPECIALIZATION:
 
High-Angle-of-Attack Aerodynamics, Flapping-Wing Aerodynamics, Transonic Flows
 
PROFESSIONAL EXPERIENCE:
 
Researcher (2002-)
Department of Mechanical and Aerospace Engineering, University of California, Irvine, CA

Visiting Professor (1990-1996)
Department of Aerospace Engineering, University of Southern California (USC), Los Angeles, CA

Visiting Professor (April-September, 1987)
Department of Mechanical Engineering, Santa Clara University, Santa Clara, CA

Visiting Professor (December 1986-March 1987)
Department of Engineering Science, California Institute of Technology (Caltech), Pasadena, CA

Visiting Professor (September-November 1986)
Mathematical Science Institute and Sibley School of Mechanical and Aerospace Engineering, Cornell University (Cornell), Ithaca, NY

Visiting Professor (June-August 1986)
Institute for Physical Science and Technology, University of Maryland (UM), College Park, MD

Professor (1970-1997)
Northwestern Polytechnical University (NPU), Xi'an, PRC

Vice-President (1979-1984)
NPU

Director (1979-1985)
Aerodynamics Research Institute, NPU

Adjunct Professor (1980-)
Shanghai Jiaotong University, Shanghai, PRC

Professor (1952-1970)
Harbin Institute of Technology, Harbin, PRC

Research Fellow (1951-1952)
Mathematics Institute, China Science Academy, Beijing

SELECTED HONORS AND AWARDS:
 
  1. Award for Major Significant Scientific and Technological Contributions, the State Science Assembly, 1978
  2. Listing of The Encyclopedia Sinica, Volume of Aeronautics and Astronautics, 1985, p. 3, 373, Encyclopedia Sinica Press, Beijing, Shanghai
  3. Certificate of Merit for Distinguished Service to The Aviation Education, Ministry of Aviation Industry, PRC, 1985
  4. Honorary Director, Chinese Society of Aeronautics and Astronautics, 1988
  5. Outstanding-Contribution Expert, Ministry of Aviation and Space Industry, PRC, 1992
  6. Outstanding Speaker, Chinese-American Engineers and Scientists Association, 1987
  7. NASA ARC Award number NCA 2-201 with T.L. Holst at Santa Clara University, Santa Clara, CA, 1987
  8. National Science Foundation U.S.-China Cooperative Research Award number 9017252, with H.K. Cheng, Department of Aerospace Engineering, USC, 1990-1993
  9. Listing of Who's Who in Science and Engineering, Premier Edition, 1992-1993, p. 527, Marquis Who's Who, A Reed Reference Publishing Company, USA
  10. Ou Jou Yi Scholarship, Taiwan, 1993
  11. Distinguished Professor, NPU, 1997

MEMBERSHIP AND LEADERSHIP IN ASSOCIATIONS:
 
  1. Member, American Mathematical Society, 1991
  2. Faculty Member, Sigma-Phi-Delta Engineering Fraternity, 1997
  3. Reviewer, Mathematical Reviews, USA, 1986
  4. Advisory Editor, Computer Methods in Applied Mechanics and Engineering, Germany, 1980-1996
  5. Director, Chinese Society of Theoretical and Applied Mechanics, 1978-1990
  6. Director, Chinese Society of Aeronautics and Astronautics, 1978-1988
  7. Director, Chinese Aerodynamics Research Society, 1980-1990
  8. Editor, Acta Aeronautica et Astronautica Sinica, 1978-1990
  9. Vice Editor in Chief, Acta Aerodynamica Sinica, 1981-1990
  10. Organizer in Chief, 1st-5th Symposium on Transonic Flows, China, 1981-1990
  11. Organizer in Chief, Conference on Aerodynamics of Aircraft Components, China, 1983

SELECTED PUBLICATIONS:
 

REFEREED JOURNAL ARTICLES:
 
  1. Liu, F., Luo, S.J., Gao, C., Meng, X.S., Hao, J.N., Wang, J.L. and Zhao, Z.J. Flow Control over a Conical Forebody Using Duty-Cycled Plasma Actuators, AIAA Journal, Vol. 46, No. 11, Nov. 2008, pp. 2969-2973
  2. Cai, J.S., Tsai, H-M, Luo, S.J. and Liu, F. Stability of Vortex Pairs over Slender Conical Bodies: Analysis and Numerical Computation, AIAA Journal, Vol. 46, No.3, March 2008, pp. 712-722
  3. Cai, J.S., Luo, S.J. and Liu, F. Stability of Symmetric and Asymmetric Vortex Pairs over Conical Wing-Body Combinations, AIAA Journal, Vol. 44, No.7, July 2006, pp. 1601-1608
  4. Gao, C., Yang, S.C., Luo, S.J., Liu, F. and Schuster, D.M. Calculation of Airfoil Flutter by an Euler Method with Approximate Boundary Conditions, AIAA Journal, Vol. 43, No. 2, Feb. 2005, pp. 295-305
  5. Cai, J.S., Luo, S.J. and Liu, F. Stability of Symmetric and Asymmetric Vortex Pairs over Slender Conical Wings and Bodies, Physics of Fluids, Vol. 16, No. 2, Feb. 2004, pp. 424-432
  6. Cai, J.S., Liu, F. and Luo, S.J. Stability of Symmetric Vortices in Two Dimensionals and over Three-Dimensional Slender Conical Bodies, Journal of Fluid Mechanics, Vol. 480, 10, April 2003, pp. 65-94
  7. Gao, C., Luo, S.J. and Liu, F. Numerical Solution of the Unsteady Euler Equations for Airfoils Using Approximate Boundary Conditions, Acta Mechanica Sinica, Vol. 19, No. 5, 2003, pp. 427-436
  8. Luo, S.J., and Wang, L.X. Shock Wave in Transonic Small-Disturbance Flow, Computer Methods in Applied Mechanics and Engineering, Vol. 167, 1998, pp. 101-108
  9. Luo, S.J. and Wang, L.X. A Computational Study of the Transonic Equivalence Rule with Lift, Journal of Aircraft, Vol. 35, No. 1, Jan-Feb. 1998, pp. 39-45
  10. Luo, S.J. and Cheng, H.K. Second-Order Small-Disturbance Solution for Wing at Supersonic Speeds, AIAA Journal, Vol. 34, No. 12, Dec. 1996, pp. 2562-2568
  11. Cheng, H.K. and Luo, S.J. On The Transonic Equivalence Rule Involving Lift and Shocks, AIAA Journal, Vol. 34, No. 5, May 1996, pp. 1080-1083
  12. Zhang, W., Luo, S.J. et al. Computer Simulation of Vortex Flows around a Body of Revolution at High Angles of Attack and Low Speed, Computer Methods in Appl. Mech. and Engng., Vol. 96, 1992, pp. 351-360
  13. Zhang, W., Luo, S.J. et al. Numerical Simulation of Vortex Breakdown Onset, Intern. J. Engng. Sci., Vol. 29, 1991, pp. 237-242
  14. Luo, S.J. and Bao, Y. Computation of Transonic Aerodynamically Compensating Pitot Tube, Journal of Aircraft, Vol. 25, No. 6, June 1988, pp. 544-547
  15. Shen, K. Y. and Luo, S.J. A Second Order Approximate Method for Transonic Small-Disturbance Potential Flow and Its Application to the Analysis of Flows over Airfoils, Computer Methods in Appl. Mech. and Engng., Vol. 49, 1985, pp. 149-161
  16. Luo, S.J., Zheng, Y.W., Qian, H. and Wang, D.Q. Finite Difference Computation for Transonic Steady Potential Flow, Computer Methods in Appl. Mech. and Engng., Vol. 27, 1981, pp. 129-138
  17. Zhu, P.Y. Shou, W.X. and Luo, S.J. Nonlinear Prediction of Subsonic Aerodynamic Loads on Wings and Bodies at High Angles of Attack, Computer Methods in Appl. Mech. and Engng., Vol. 26, 1981, pp. 305-319
  18. Pai, S.I. and Luo, S.J. Theoretical and Computational Dynamics of A Compressible Flow, 699 pp., 1991, Van Nostrand Reinhold, NY and Science Press, Beijing
  19. Luo, S.J. et al. Mixed Difference Methods for Steady Transonic Potential Flows, 154 pp., 1979, National Defense Industry Press, Beijing (in Chinese)

ARCHIVED CONFERENCE PAPERS:
 
  1. Liu, F., Luo, S.J., Gao, C., Wang, J.L., Zhao, Z.J., Li, Y.Z. and Hao, J.N. Mechanisms for Conical Forebody Flow Control Using Plasma Actuators, AIAA 2009-4284, Jun. 2009
  2. Liu, F., Luo, S.J., Gao, C., Meng, X.S., Hao, J.N., Wang, J.L. and Zhao, Z.J. Flow Control over a Conical Forebody Using Duty-cycled Plasma Actuators, AIAA 2009-1082, Jan. 2009
  3. Wang, J.L., Li, H.X., Liu, F. and Luo, S.J. Forebody Asymmetric Load Manipulated by a Horseshoe-Shaped Plasma Actuator, AIAA 2009-0904, Jan. 2009
  4. Zhao, Z.J., Li, H.X., Liu, F. and Luo, S.J. Forward-Blowing Plasma Actuation over Forebody Asymmetric Vortex, AIAA 2009-0752, Jan. 2009
  5. Meng, X.S., Qiao, Z.D., Gao, C., Luo, S.J. and Liu, F. Asymmetry Features Independent of Roll Angle for Slender Circular Cone, AIAA 2009-0905, Jan. 2009
  6. Meng, X.S., Qiao, Z.D., Gao, C., Luo, S.J. and Liu, F. Flow over Delta Wing with Low Dorsal Fin--PIV Study, AIAA 2009-0541, Jan. 2009
  7. Meng, X.S., Qiao, Z.D., Gao, C., Luo, S.J. and Liu, F. Reynolds Number Effects on Cone Forebody Side Force, AIAA 2008-4033, June 2008
  8. Jia, C., Meng, X.S., Qiao, Z.D., Gao, C., Luo, S.J. and Liu, F. Pressure around a 20-Degree Circular Cone at 35-Degree Angle of Attack and Low Speed, AIAA 2007-4453, June 2007
  9. Meng, X.S., Jia, C., Qiao, Z.D., Gao, C., Luo, S.J. and Liu, F. Development of Flow Asymmetry over a 20-Degree Circular Cone at Low Speed, AIAA 2007-4418, June 2007
  10. Yang, S.C., Luo, S.J., Liu, F. and Tsai, H-M. Euler Solutions of Flow around a Rectangular Wing with Square Tip, AIAA 2007-0896, Jan. 2007
  11. Meng, X.S., Jia, C., Qiao, Z.D., Gao, C., Luo, S.J. and Liu, F. Aerodynamic Characteristics of Slender Delta Wing with Low Dorsal Fin, AIAA 2007-1272, Jan. 2007
  12. Yang, S.C., Luo, S.J., Liu, F. and Tsai, H-M. Trailing-Edge Flow about Unstalled Plunging Airfoil Computed by Euler Method, AIAA 2006-3209, June 2006
  13. Cai, J.S., Tsai, H-M., Luo, S.J. and Liu, F. Design of Wing-Body Configurations to Delay the Onset of Vortex Asymmetry, AIAA 2006-3319, June 2006
  14. Yang, S.C., Luo, S.J., Liu, F. and Tsai, H-M. Subsonic Flow over Unstalled Pitching Airfoil Computed by Euler Method, AIAA 2006-3914, June 2006
  15. Yang, S.C., Luo, S.J., Liu, F. and Tsai, H-M. Optimization of Unstalled Pitching and Plunging Motion of an Airfoil, AIAA Paper 2006-1055, Jan. 2006
  16. Yang, S.C., Luo, S.J., Liu, F. and Tsai, H-M. Supercritical Flow over Unstalled Plunging Airfoil Computed by Euler Method, AIAA Paper 2006-0293, Jan. 2006
  17. Meng, X.S., Qiao, Z.D., Gao, C., Luo, S.J. and Liu, F. Visualization of Vortex Flow over Delta Wing with Dorsal Fin, AIAA Paper 2005-1058, Jan. 2005
  18. Cai, J.S., Tsai, H-M., Luo, S.J. and Liu, F. Vortex Core and Its Effects on the Stability of Vortex Flow over Slender Conical Bodies, AIAA Paper 2005-0062, Jan. 2005
  19. Yang, S.C., Luo, S.J., Liu, F. and Tsai, H-M. Computation of the Flow over Flapping Airfoil by Euler Equations, AIAA Paper 2005-1404, Jan. 2005
  20. Yang, S.C., Liu, F., Luo, S.J., Tsai, H-M. and Schuster, D.M. Time-domain Aeroelastic Simulation on Stationary Body-Conforming Grids with Small Perturbation Boundary Conditions, AIAA Paper 2004-0885, Jan. 2004
  21. Yang, S.C., Liu, F., Luo, S.J., Tsai, H-M. and Schuster, D.M. Three-Dimensional Aeroelastic Computation Based on Stationary Body-Conforming Grids with Small Perturbation Boundary Conditions, AIAA Paper 2004-2235, June 2004
  22. Yang, S.C., Zhang, Z.C., Liu, F., Luo, S.J., Tsai, H-M. and Schuster, D.M. Time-Domain Aeroelastic Simulation by a Coupled Euler and Integral Boundary-Layer Method, AIAA Paper 2004-5377, Aug. 2004
  23. Cai, J.S., Tsai, H-M, Luo, S.J. and Liu, F. Stability of Vortex Pairs over Slender Conical Bodies-Theory and Numerical Computations, AIAA Paper 2004-1072, Jan. 2004
  24. Cai, J.S., Tsai, H-M, Luo, S.J. and Liu, F. Control of Vortices over Slender Conical Bodies - A Theoretical and Computational Study, AIAA Paper 2004-2416, June 2004
  25. Cai, J.S., Luo, S.J. and Liu, F. Stability of Symmetric and Asymmetric Vortex Pairs over Slender Conical Wings and Bodies, AIAA Paper 2003-1101, Jan. 2003
  26. Cai, J.S., Luo, S.J. and Liu, F. Stability of Symmetric and Asymmetric Vortex Pairs over Slender Conical Wing-Body Combinations, AIAA Paper 2003-3598, June 2003
  27. Cai, J.S., Liu, F. and Luo, S.J. Stability of Symmetric Vortices behind Two-Dimensional Bodies, AIAA Paper 2001-2844, June 2001
  28. Cai, J.S., Liu, F. and Luo, S.J. Stability of Symmetric Vortices over Slender Conical Bodies at High Angles of Attack, AIAA Paper 2001-2845, June 2001
  29. Cai, J., Tsai, H-M., Luo, S. and Liu, F. Study of Stability of Vortex Pairs over a Slender Conical Body by Euler Computations, in Frontiers of Computational Fluid Dynamics 2006, ed. D.A. Caughey and M.M. Hafez, World Scientific, 2006, pp.297-323
  30. Luo, S.J., Shen, H.L. and Liu, P. Transonic Small Transverse Perturbation Equation and Its Computations, Proc. Symposium on Computing the Future II: Computational Fluid Dynamics Advances and Applications, June 24-26, 1997/Everett, WA
  31. Luo, S.J. and Zhang, W. Computer Simulation of Low Speed Vortical Flow around Body of Revolution at High Angles of Attack, Keynote Speech, Intern. Conference on Modeling and Simulation, Shenzhen, November 7-9, 1988
  32. Li, X.Y., Liao, Q.W. and Luo, S.J. A Parallel Algorithm of AF-2 Scheme for Plane Steady Transonic Potential Flow with Small Transverse Disturbance, ICAS- 88-4.7.1, Proc. 16th Congress of the Intern. Council of the Aeronautical Sciences, Jerusalem, Israel, August 28-September 2, 1988, pp. 1024-1028
  33. Wang, L.X. and Luo, S.J. Numerical Solution of Transonic Small Disturbance Pressure Equation and Its Applications, Proc. 10th Intern. Conference on Numerical Methods in Fluid Dynamics, Beijing, June 23-27, 1986; Lecture Notes in Physics 264 (1986) pp. 636-641
  34. Li, X.Y. and Luo, S.J. Finite Difference Computation of Pressure and Wave Drag of Slender Bodies of Revolution at Transonic Speeds with Zero-Lift, Proc. 8th Intern. Conference on Numerical Methods in Fluid Dynamics, Aachen, Germany, June 28-July 2, 1982; Lecture Notes in Physics, 170 (1982) pp. 350-356

INVITED INTERNATIONAL LECTURES:
 
  1. A Transonic Small Transverse Perturbation Equation and Its Computation, W.M. Reed Mech. Eng. Seminar, Department of Mechanical Engineering, University of Kentucky, Lexington, KY, October 6, 1995
  2. An Analytical Solution of Second-Order Small-Disturbance Equation for Three-Dimensional Wings at Supersonic Speeds, Monday Research Conference, Department of Aerospace Engineering, USC, April 19, 1993
  3. Transonic Small Transverse Perturbation Equation, Aerospace and Mechanical Engineering Colloquium, San Diego State University, San Diego, CA, March 26, 1992
  4. A Transonic Small Transverse Perturbation Equation and Its Computation, Seminar MA 200A, Department of Mechanical and Environmental Engineering, University of California, Santa Barbara, CA, June 3, 1991
  5. Course Lectures on Aerodynamics of wings and Bodies, Fall Semester, USC, 1990 and 1991
  6. Course Lectures on Current Topics in Aerodynamics, Spring Semester, USC, 1990
  7. Computer Simulation of Low Speed Vortical Flow around Body of Revolution at High Angles of Attack, Keynote Speech, Intern. Conference on Modeling and Simulation, Shenzhen, November 7-9, 1988
  8. A Transonic Small Transverse Perturbation Equation and Aerospace Engineering in China, Faculty Research Seminar, Department of Mechanical Engineering, Santa Clara University, May 26, 1987
  9. Research and Development of Aerodynamics and Aerospace Industry in PRC, 1987 Technical Conference and Industrial Exhibition, Chinese-American Engineers and Scientists Association of Southern California, Los Angeles, CA, March 21, 1987
  10. A Transonic Small Transverse Perturbation Equation and Its Computation, Fluid Dynamics Seminar, Caltech, February 27, 1987
  11. Convergence and Stability of Steady Transonic Small Perturbation Equation Computations, Special Applied Mechanics Seminar, School of Engineering and Department of Mathematics, USC, February 17, 1987
  12. Uniqueness of Difference Solution of Transonic Small Perturbation Equation, Applied Mathematics Colloquium, University of California at Los Angeles, Los Angeles, CA, February 10, 1987
  13. A Series of 8 Seminar Lectures on Computation of Transonic Small Perturbation Flow, Mathematical Science Institute and Sibley School of Mechanical and Aerospace Engineering, Cornell, September 30-November 25, 1986
  14. A Transonic Small Transverse Perturbation Equation and Its Computation, Aerospace Engineering Seminar, UM, July 1 and 24, 1986
  15. A Series of 4 Seminar Lectures on Computation of Transonic Small Perturbation Flows, The Aeronautical Research Institute of Sweden (FFA), Royal Institute of Technology and Saab-Scania, Sweden, November 1-13, 1982

MASTER'S SUPERVISIONS:
 
  1. Jia C. Thesis: Mechanism for Separation Vortex Asymmetry over Slender Conical Bodies at High Angles of Attack, 2007. Co-Supervisor: Gao, C. and Liu, F.
  2. Meng, X.S. Thesis: Effects of Dorsal Fin on Stability of Vortices over Slender Flat-Plate Delta Wing, 2005. Co-Supervisor: Qiao, Z.D. and Liu, F.
  3. Li, L.G. Thesis: Axisymmetric Magnetic Field of Magnetic Suspension and Balance System and Numerical Computation of Magnetic Forces, 1990. Co-Supervisor: Ji, S.P.
  4. Zheng, Y.Y. Thesis: Finite Volume Method for Transonic Steady Flows, 1989
  5. Cai, J.S. Thesis: Computerized Derivation of Formulae and Transonic Aerodynamic Prediction of Space Shuttle, 1989
  6. Liao, Q.W. Thesis: A Parallel Algorithm of AF-2 Scheme for Steady Transonic Potential Flow about Airfoils, 1989. Published papers: (1) Acta Aerodynamica Sinica 4 (1986) 313-319; (2) ICAS-88-4.7.1 (1988) 1024-1028. Co-Supervisor: Li, X.Y.
  7. Min, S.J. Thesis: An Efficient Parallel Algorithm of AF-2 Scheme for Steady Axisymmetric Transonic Flows on Computer YH-1, 1989. Published papers: (1) Acta Aeronautica et Astronautica Sinica 8 (1987) A518-523; (2) Acta Aeronautica et Astronautica Sinica 11 (1990) A510-A514; (3) Chinese Journal of Computational Physics 7 (1990) 241-249; (4) Numerical Computation and Computer Application (1992) No.2. Co-Supervisor: Li, X.Y.
  8. Qian, C. Thesis: A Flow Visualization Water Tunnel and Study of Vortical Flows about a Delta Wing, 1989
  9. Yang, Y.K. Thesis: AF-2 Computation of the Interior and Exterior Axisymmetric Flows about Pitot-Type Inlet, 1988. Published paper: Acta Aerodynamica Sinica 7 (1989) 123-129. Co-Supervisor: Shen, H.L.
  10. Chai, Z.J. Thesis: A Boundary-Layer Code Coupled with the Bauer-Garabedian-Korn Inviscid Code for Supercrical Wing Sections, 1987, Co-Supervisor: Shen, K.Y.
  11. Ang, H.S. Thesis: Calculation of Unsteady Transonic Flows with Large Longitudinal Disturbance, 1986
  12. Gao, C. Thesis: Effects of Suction at side Wall around Models in a Transonic Airfoil Wind Tunnel, 1986. Published paper: Acta Aeronautica et Astronautica Sinica 8 (1987) A274-A278
  13. Liu, P. Thesis: Iterative Computation of Transonic Potential Flow past Airfoils with Boundary Layer, 1986. Published papers: (1) Acta Aerodynamica Sinica 4 (1986) 279-288; (2) 1st World Congress Comp. Mech. Sep 22-26 1986
  14. Bao, Y. Thesis: A Simplified Method of Computing Transonic Flow around Bodies of Revolution at Non-Zero Angles of Attack, 1985. Published papers: (1) Acta Aeronautica et Astronautica Sinica 8 (1987) B287-B290; (2) Acta Aerodynamica Sinica 5 (1987) 326-333; (3) AIAA Paper 87-2613 (1987)
  15. Wang, L.X. Thesis: Numerical Solution of Transonic Small Disturbance Pressure Equation Using a Mixed Difference Method, 1985. Published papers: (1) Acta Aerodynamica Sinica 4 (1986) 159-167; (2) Acta Aeronautica et Astronautica Sinica 8 (1987) A103-A109; (3) Lecture Notes in Physics 264 (1986) 636-641
  16. Liu, X.D. Thesis: On Relaxation of Transonic Flows around Zero-Lift Airfoil and Convergence of Self-Correcting Wind Tunnels, 1984. Published paper: Acta Aerodynamica Sinica (1984) No.3, 34-41
  17. Li, X.Y. Thesis: Finite Difference Computation of Wave Drag and Pressure on Slender Bodies of Revolution at Transonic Speeds with Zero-Lift, 1983. Published papers: (1) Acta Aeronautica et Astronautica Sinica 4 (1983) 20-28; (2) Lecture Notes in Physics, 170 (1982) 350-356
  18. Zheng, Y.W. Thesis: Relaxation Computation of Transonic Flows around Wings with Blunt Leading Edge, 1983. Published papers: (1) Acta Aeronautica et Astronautica Sinica 3 (1982) 1-14; (2) Acta Aerodynamica Sinica (1983) No.2, 20-28; (3) Computer Meth. Appl. Mech. Engng. 27 (1981) 129-138

DOCTORAL SUPERVISIONS:
 
  1. Meng, X.S. Thesis: Asymmetric Vortices Characteristics Study and Flow Control of Slender Body at High Angles of Attack, 2008. Co-Supervisor: Qiao, Z.D. and Liu, F.
  2. Zhong, C.W. Thesis: Numerical Simulation of Separated Flow around Transonic Wings by Viscous/Inviscid Interaction Technique, 1997, Co-Supervisor: Su, Y.X.
  3. Gao, C. Thesis: Transonic Second-Order Approximation Theory and Numerical Calculation of Vortical Flow at High Angles of Attack, 1995, Co-Supervisor: Yang, Y.
  4. Zhang, Z.K. Thesis: Multi-Grid Numerical Solutions of Euler Equations of Transonic Flow around Wing-Body Combination at High Angles of Attack, 1994, Co-Supervisor: Li, F.W.
  5. Li, L. Thesis: Numerical Analysis of Transonic Flows by Viscous/Inviscid Interaction Technique, 1994, Co-Supervisor: Li, F.W.
  6. Li, H.X. Thesis: Study on Flexible Self Adaptive Wall Wind Tunnel of Three-Dimensional Flows, 1993, Co-Supervisor: He, J.J.
  7. Cai, J.S. Thesis: Numerical Simulation of Transonic High Angle of Attack Flow around Wings and Bodies by Euler Equations, 1992, Co-Supervisor: Li, F.W.
  8. Liu, P. Thesis: Numerical Methods of Transonic Flow around Airfoils and Wings and Their Applications, 1989
  9. Bao, Y. Thesis: Calculations of Transonic Small Disturbance Potential Flows around the Wing-Body-Pylon-Store Combinations and Two-Dimensional Steady Transonic Euler Flows, 1988
  10. Zhang, W. Thesis: Computation of the Vortical Flow around Body of Revolution at High Angles of Attack and Low Speeds, 1988
  11. Zhou, M.D. Thesis: Theoretical and Experimental Investigation on Blowing Trailing-Edge Flap of a Swept-Back Wing, 1966
  12. Zhuang, L.X. Thesis: Theoretical and Experimental Investigation on the Problem of Optimum Cambering and Twisting of Delta Wings at Subsonic Speeds, 1965

POST-DOCTORAL SUPERVISIONS:
 
  1. Fang, J.Y. Published paper: Computation of subsonic non-linear loads on flat plate wings at high angles of attack, Computational Mechanics, Cheung, Lee and Leung eds (1991) 1543-1547
  2. Yang, S.C. 2003-2006



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On 20 June 2007