西工大的国宝---罗时钧教授今昔

恩，西工大国家的国宝...

西工大太需要这样的教授，向罗教授致敬！

传说中的东航第一才子啊！

罗今年应该是86岁。

致敬。

导师的 导师

想想当年的留学生，胡适，陈寅恪，蔡元培，郁达夫，詹天朔，想想现在的社会主义孩子，真是无语呀。后来想想还是民国时期好呀，那个时候重视人才，社会进步，知识分子地位高。

西工大太多大老板都已经不干活了，罗老师这样的导师真的值得我们敬佩。

在中国 大老板 要统筹安排，接大项目，办大事呢

罗教授是钱学森在国外的第一个弟子

国内做官才有钱途

南方好一点，在西安你必须进入这个官僚体系，才能舒舒服服

不是重视不重视人才的缘故，是那个时候没有很强的意识形态控制，人的思想都比较自由！所以大家喷薄而出，现在一个先进性就死了一大半，再戴上三块表，没被洗脑就万幸了~

1923年4月1日生于江西省南昌市。

应该是86岁

阿，江西
老乡阿
顶

康沫狂教授刚刚还在金属学报上发了2篇研究文章呢
1920年1月生，已经89高龄了

转个教授的简历吧：
Shijun Luo, aka Shih-Chun Lo
Researcher
Department of Mechanical and Aerospace Engineering
University of California, Irvine
Irvine, CA 92697-3975
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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
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AREA OF SPECIALIZATION:
High-Angle-of-Attack Aerodynamics, Flapping-Wing Aerodynamics, Transonic Flows
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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
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SELECTED HONORS AND AWARDS:
Award for Major Significant Scientific and Technological Contributions, the State Science Assembly, 1978
Listing of The Encyclopedia Sinica, Volume of Aeronautics and Astronautics, 1985, p. 3, 373, Encyclopedia Sinica Press, Beijing, Shanghai
Certificate of Merit for Distinguished Service to The Aviation Education, Ministry of Aviation Industry, PRC, 1985
Honorary Director, Chinese Society of Aeronautics and Astronautics, 1988
Outstanding-Contribution Expert, Ministry of Aviation and Space Industry, PRC, 1992
Outstanding Speaker, Chinese-American Engineers and Scientists Association, 1987
NASA ARC Award number NCA 2-201 with T.L. Holst at Santa Clara University, Santa Clara, CA, 1987
National Science Foundation U.S.-China Cooperative Research Award number 9017252, with H.K. Cheng, Department of Aerospace Engineering, USC, 1990-1993
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
Ou Jou Yi Scholarship, Taiwan, 1993
Distinguished Professor, NPU, 1997
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MEMBERSHIP AND LEADERSHIP IN ASSOCIATIONS:
Member, American Mathematical Society, 1991
Faculty Member, Sigma-Phi-Delta Engineering Fraternity, 1997
Reviewer, Mathematical Reviews, USA, 1986
Advisory Editor, Computer Methods in Applied Mechanics and Engineering, Germany, 1980-1996
Director, Chinese Society of Theoretical and Applied Mechanics, 1978-1990
Director, Chinese Society of Aeronautics and Astronautics, 1978-1988
Director, Chinese Aerodynamics Research Society, 1980-1990
Editor, Acta Aeronautica et Astronautica Sinica, 1978-1990
Vice Editor in Chief, Acta Aerodynamica Sinica, 1981-1990
Organizer in Chief, 1st-5th Symposium on Transonic Flows, China, 1981-1990
Organizer in Chief, Conference on Aerodynamics of Aircraft Components, China, 1983
************************************
SELECTED PUBLICATIONS:
REFEREED JOURNAL ARTICLES:
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
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
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
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
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
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
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
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
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
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
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
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
Zhang, W., Luo, S.J. et al. Numerical Simulation of Vortex Breakdown Onset, Intern. J. Engng. Sci., Vol. 29, 1991, pp. 237-242
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
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
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
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
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
Luo, S.J. et al. Mixed Difference Methods for Steady Transonic Potential Flows, 154 pp., 1979, National Defense Industry Press, Beijing (in Chinese)
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ARCHIVED CONFERENCE PAPERS:
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
Cai, J.S., Liu, F. and Luo, S.J. Stability of Symmetric Vortices behind Two-Dimensional Bodies, AIAA Paper 2001-2844, June 2001
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
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
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
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
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
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
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
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INVITED INTERNATIONAL LECTURES:
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
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
Transonic Small Transverse Perturbation Equation, Aerospace and Mechanical Engineering Colloquium, San Diego State University, San Diego, CA, March 26, 1992
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
Course Lectures on Aerodynamics of wings and Bodies, Fall Semester, USC, 1990 and 1991
Course Lectures on Current Topics in Aerodynamics, Spring Semester, USC, 1990
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
A Transonic Small Transverse Perturbation Equation and Aerospace Engineering in China, Faculty Research Seminar, Department of Mechanical Engineering, Santa Clara University, May 26, 1987
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
A Transonic Small Transverse Perturbation Equation and Its Computation, Fluid Dynamics Seminar, Caltech, February 27, 1987
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
Uniqueness of Difference Solution of Transonic Small Perturbation Equation, Applied Mathematics Colloquium, University of California at Los Angeles, Los Angeles, CA, February 10, 1987
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
A Transonic Small Transverse Perturbation Equation and Its Computation, Aerospace Engineering Seminar, UM, July 1 and 24, 1986
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:
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.
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.
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.
Zheng, Y.Y. Thesis: Finite Volume Method for Transonic Steady Flows, 1989
Cai, J.S. Thesis: Computerized Derivation of Formulae and Transonic Aerodynamic Prediction of Space Shuttle, 1989
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.
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.
Qian, C. Thesis: A Flow Visualization Water Tunnel and Study of Vortical Flows about a Delta Wing, 1989
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.
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.
Ang, H.S. Thesis: Calculation of Unsteady Transonic Flows with Large Longitudinal Disturbance, 1986
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
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
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)
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
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
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
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
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DOCTORAL SUPERVISIONS:
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.
Zhong, C.W. Thesis: Numerical Simulation of Separated Flow around Transonic Wings by Viscous/Inviscid Interaction Technique, 1997, Co-Supervisor: Su, Y.X.
Gao, C. Thesis: Transonic Second-Order Approximation Theory and Numerical Calculation of Vortical Flow at High Angles of Attack, 1995, Co-Supervisor: Yang, Y.
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.
Li, L. Thesis: Numerical Analysis of Transonic Flows by Viscous/Inviscid Interaction Technique, 1994, Co-Supervisor: Li, F.W.
Li, H.X. Thesis: Study on Flexible Self Adaptive Wall Wind Tunnel of Three-Dimensional Flows, 1993, Co-Supervisor: He, J.J.
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.
Liu, P. Thesis: Numerical Methods of Transonic Flow around Airfoils and Wings and Their Applications, 1989
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
Zhang, W. Thesis: Computation of the Vortical Flow around Body of Revolution at High Angles of Attack and Low Speeds, 1988
Zhou, M.D. Thesis: Theoretical and Experimental Investigation on Blowing Trailing-Edge Flap of a Swept-Back Wing, 1966
Zhuang, L.X. Thesis: Theoretical and Experimental Investigation on the Problem of Optimum Cambering and Twisting of Delta Wings at Subsonic Speeds, 1965
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POST-DOCTORAL SUPERVISIONS:
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
Yang, S.C. 2003-2006
注："*"为便于浏览而添加，转自http://luke.eng.uci.edu/sluo/index.html

汗颜呀
牛人呀
同样是东航的林超强同学谁接着发下

老乡啊！！

好荣幸啊！

有幸得到罗老的一本书，幸甚！

这不中央大学吗？

 

就是当年的中央大学。现在在国内叫南京大学，在台湾还是叫中央大学

B.S., 1945, Department of Aeronautical Engineering,
National Central University, Chongqing, China
中大，是中国人的中大！

虽然不懂他老人家的研究领域，但对有真才实学的人，一直十分钦佩。
四年的大学时光就将结束，没有福气见到品德高尚、学术精湛的好老师，倍感遗憾。

现在的留学生大都是花钱的。。。

罗时钧
（１９２３年— ）
罗时钧，空气动力学家、力学教育家。长期从事跨声速空气动力学与大迎角空气动力学的教学和研究工作，较早将计算流体力学应用于我国的超声速飞机设计，在大迎角气动力计算方面取得了重要成果。
　　罗时钧，１９２３年４月１日出生于江西省南昌市一个书香门第家庭。在家庭的熏陶下，他从小饱读诗书。当时中国国力衰微，民不聊生，科学落后，日本侵略军的飞机大炮狂轰滥炸，这一切深深地刺伤了少年罗时钧的民族自尊心，他由此立下了“科学救国”的志向。１９４１年，他以优异的成绩考入重庆中央大学航空工程系。１９４５年，在该校获航空工程学士学位。由于品学兼优，被留校任助教。１９４７年９月考入美国明尼苏达大学航空工程系，１９４８年８月获航空工程硕士学位，同年９月考入美国加利福尼亚理工学院航空系攻读博士学位，主修空气动力学，副修数学，导师是著名科学家钱学森，１９５０年９月获得航空数学哲学博士学位。由于急于学成归国，报效祖国，罗时钧在美就学期间抓紧分秒的学习时间，连假期都不曾外出游玩，因而在一年内即攻下了硕士学位；接着两年内又攻下了博士学位。此时中华人民共和国刚刚诞生不久，这片倍遭战乱摧残的、养育了他的土地，深深地吸引着这位年仅２７岁的、已学贯中西的青年学者。还在他毕业之前，他和他的导师钱学森及加州理工学院的留美同仁赵忠尧、沈善炯等就计划着要返回祖国大陆，他们几经周折，于１９５１年１月返回祖国。
　　回国后，罗时钧被安排在中国科学院数学研究所从事力学研究工作。１９５２年，我国第一个军事工程学院在哈尔滨组建，罗时钧听从派遣，于１９５２年１１月奔赴当时生活条件很艰苦的哈尔滨中国人民解放军军事工程学院，和岳毅等组建空气动力学教研室。当时国内空气动力学专业没有中文教材，罗时钧经过几年的教学实践，于１９５５至１９５６年编写了我国第一部空气动力学讲义，以后又相继编写了多部空气动力学专业教材，教育、培养了几代空气动力学人才。１９５８年，他为中国的第一架新型超声速飞机设计提出了气动力计算方案，并指导学生用手摇计算机完成了这一计算。
　　“文化大革命”期间，罗时钧身心及其家庭受到了摧残，在那倍受磨难的年月里，他仍怀着爱国的赤子之心，在极端困难的条件下，坚持他所热爱的科研工作。１９７０年，哈尔滨军事工程学院航空系并入西北工业大学，罗时钧也随之转到西北工业大学。他争分夺秒地工作，率先开展了跨声速空气动力学的研究，在国内首次将有限差分方法用于飞机空气动力计算。７０年代，他主持并完成跨声速－机翼－平尾－立尾组合体纵向空气动力差分计算程序，获１９７７年陕西省科研成果奖，被选入１９７７年全国国防科研成果展览。１９７８年，他参加全国科学大会，获科研成果奖和先进工作者奖。１９７６年，在国内首次解决了大迎角非线性气动力计算的收敛性问题。１９８８年，将计算迎角提高到６０°，在国际上首次得到大迎角非对称气动力计算结果。１９８３年，合作研究了跨声速小扰动速势流二级近似方法及其在翼型和机翼绕流计算上的应用，获航空工业部理论成果奖。１９８６年，合作研究了Ｓ形进气道流场的计算机模拟，获陕西省高校科研成果二等奖。他曾应邀去瑞典皇家工学院、联邦德国宇航院、美国康奈尔大学、马里兰大学、加州理工学院、南加州大学等十几所国外大学、研究所，进行科学研究和讲学活动，并协助建立了西北工业大学和联邦德国宇航院的科技协作关系。由于他的积极推荐，使得一批空气动力专业的年轻科研骨干能赴联邦德国、瑞典学习深造并进行科技合作。罗时钧从空气动力学学科发展的高度出发，指出“自修正风洞”是一个重要研究方向，指导研究生进行了这方面的探讨，并敦促空气动力学研究室将这一工作深入下去，使得这一课题取得较丰硕的研究成果，在国内外均受到了关注。
　　罗时钧先后受聘为上海交通大学兼职教授，昆明云南工学院名誉教授，长沙国防科大兼职教授，美国马里兰大学、康奈尔大学、加州理工学院、圣他克罗那大学、南加州大学访问教授；航空航天部干线飞机总设计师顾问；美国《数学评论》学会评论员，联邦德国《应用力学与工程中的计算机方法》顾问、编委，《航空学报》、《力学进展》编委，《空气动力学学报》副主编。他还是中国力学学会理事，中国航空学会理事、名誉理事，中国空气动力学研究会理事，全国第一、第二、第三、第四、第五届跨声速流学术讨论会组织委员任委员。曾任航空工业部科学技术委员会委员、国家科委理论与应用力学学科组组员、中国科学院技术科学部工程力学分组成员、黑龙江省人民代表、陕西省政协委员。
　　罗时钧长期从事飞机部件空气动力学、跨声速空气动力学、大迎角空气动力学的教学和研究工作，４０年来一直奋斗在教学科研第一线，为我国培养了大批流体力学方面的专门人才，先后指导硕士、博士研究生几十名，其中有些已成为国内知名学者。罗时钧为我国航空教育与科研事业作出了重大贡献。
赤子之心
１９５０年，他在美国加州理工学院提前完成了学位论文，获得了博士学位。这时，中华人民共和国成立不久，人民政府号召海外学者返回自己的祖国参加建设，这对罗时钧是一个巨大的吸引力。在导师钱学森的鼓励下，于同年８月３１日和赵忠尧、沈善炯一行３人毅然踏上了回国的道路。他们乘船离开美国西海岸，于９月１２日到达日本的横滨港。
这一年６月，朝鲜战争爆发，当他们３人到达横滨时，就被在日本的美国占领军逮捕，关进了巢鸭监狱，罪名是所谓携带有关国防秘密资料。１２月初，又被转送到东京麻布区的“中国驻日代表团”驻地，即当时的国民党驻日“大使馆”，国民党官员劝说他们回美国去，或是到台湾，并说台大校长傅斯年已从台湾来电，聘请他们任台大教授，对此，他们都断然拒绝，理直气壮地回答：“中国是我的祖国，我为什么不能回去？”最后，美军抓不到任何证据，迫于舆论的压力，只好放人，这时已是１２月下旬。罗时钧和他的两位同伴就是这样，怀着一颗热爱祖国、报效祖国的赤诚之心，历经磨难，投入到了祖国的怀抱。
　　在“文化大革命”期间他被说成是“派谴特务”，受到了严刑逼供，身上多处伤残，受尽了种种折磨和极不公正的待遇。妻子也被逼死，……但是，他对祖国的赤诚之心不变，对党的信念不变。他说，他永远相信党，胡做非为的是少数人。
　　正是在这种波折中，他的爱国之心又得到了升华，由爱国、爱党到下定决心为党的事业奋斗终生。他多次递交入党申请书，表示要把自己的一切交给党。１９７８年，他参加了全国科学大会，并获了奖，他内心的激动难以言表，因为他所做的工作得到了党的支持和鼓励。
　　１９８０年，他光荣地加入了中国共产党。从此，他全身心地投入到社会主义建设中去。他常说，“文化大革命”１０年，我们与发达国家相比，差距不是缩小了，而是扩大了，我们要加倍工作，把损失的时间弥补过来，努力把我国的航空事业搞上去。
　　如今，他已年近古稀，但是，他仍旧在竭尽全力报效祖国。
刻苦攻关
　　５０年代初，他到哈尔滨军事工程学院任教。他讲的课是全院有名的样板课，学生们反映，罗教员讲课思路清晰、语言精炼、概念明确。因而，院、系多次组织对他的课进行观摩、学习。在讲课的基础上，经过加工、整理，他编写出了自己的空气动力学讲义。以后，又陆续编写了空气动力学讲义续篇，包括机翼的理论和应用、细长体的理论和应用。这些，不仅大大丰富了教学，也为我国飞行器空气动力学的科学研究与设计提供了十分有价值的参考资料。
　　“文化大革命”时期，他为我国航空事业受到干扰、破坏而焦急，他不怕打击，只是一心把自己的工作和祖国的前途、社会主义事业的发展紧密联系在一起。他深深地体会到，教学、科研工作必须与厂、所的设计和生产密切结合。于是他选择了这一最困难的方向。
　　７０年代初，他开始探讨空气动力计算中的一个难点——跨声速空气动力研究。当飞行器作跨声速飞行时，即这时的速度相当于声音传播的速度，大约在０．８—１．２倍声速的范围内，此时绕飞行器的流动是比较复杂的，它包含亚声速气流和超声速气流的混合流动，而且存在着激波。在理论上虽然早已建立了描述这一流动的跨声速气流的速势方程，但这是一种非线性的混合型偏微分方程，不能用一般的纯亚声速、纯超声速的线性迭加的方法求解。罗时钧知道，不论对民用飞机还是军用飞机，跨声速都是一个重要的飞行速度范围，因此，分析、计算跨声速时飞行器的空气动力性质对飞行器的设计是至关重要的。然而，怎样解非线性偏微分方程？工程方法太粗糙，风洞实验在我国当时的条件下，经费和时间都不允许，为此，他查阅了大量的国外资料，从中受到启发，决定对跨声速混合差分法进行探索，利用电子计算机作数值计算来求解跨声速速势方程。这种数值计算方法，在某些人看来，是一件繁琐无味的“流汗”的事情，没有什么高深的理论可研究，他却认为，只要是生产实际中的问题，只要对解决实际的飞行器空气动力问题有帮助，“流汗”再多也值得。
　　当时他已是年过半百的人了，为了利用合适的计算机，他经常出差在外，工作起来常常废寝忘食，有一种不达目的决不罢休的顽强精神。他总是和程序人员一起上机，守在计算机旁，对数据做现场分析，指导进一步的计算，中午他也不离开机房，吃点冷馍、咸菜就算是午饭了。１９７６年，他那在“文化大革命”中受伤的小腿再次发炎，１９７７年颈部脂肪瘤发炎，他都是一面打针吃药，一面坚持全天工作，甚至晚上也不休息。为了争取时间，有两个春节都是在外地度过的。经过几年的艰苦劳动，他在跨声速空气动力课题方面取得了可喜的成果，完成了通用的计算程序。采用这一计算方法，可以提高飞行器设计的质量，缩短研制周期，降低成本。这一成果填补了我国航空技术上的一项空白，也接近当时国外的研究水平。
　　８０年代，他又开始了大迎角课题的研究。由于飞行器在大迎角飞行时，气流不再沿飞行器表面光滑地流过，而是产生分离流动并形成旋涡。这样的分离涡流在飞行器的左、右往往会出现不对称的现象，而且，还会发生涡的破裂，这种十分复杂的流动给分析和计算带来了困难。他从７０年代末开始研究大迎角时的流动特性和计算方法，与他人合作，在国内首先解决了大迎角空气动力数值计算的收敛性问题，１９８８年，又将计算迎角提高到６０°，在国际上首次得到大迎角非对称气动力计算结果，在计算方法上取得了突破，具有较高的理论和应用价值。
教书育人
由于他的学术水平高，在国内外同行中有很高的声望。但是，他总是严格要求自己，以自己的一言一行实现着报效祖国的志向，同时，也教育着他的一代又一代的学生。
近１０多年来，他先后培养了几十名研究生。他对学生不仅严格要求，更是循循善诱。在指导研究生时，他总是那样认真、细致，不仅关心学生的业务进步，而且帮助学生在思想上提高。他说过，我就是这么一点知识，不交给学生，不交给国家，难道还要带进棺材吗？
　　改革开放初期，国外就有人邀请他出国讲学，但是他考虑，最重要的是多做一些培养教育年轻人的工作，有出国的机会让年轻一些的同志先出去进修吧！就这样，他一直到１９８６年才应邀到美国访问。在访美期间，他一方面介绍我国在空气动力学研究方面的成就，一方面抓紧时间，汲取国外的新技术。他经常主动地将国外技术发展的最新信息及时告诉国内的有关同志。他时刻想的都是祖国航空事业的发展。
　　人们都说“罗老师是一心搞学问的人”，但他对学生、对其他同志却十分关心。研究室有一位实验技术人员的家属生病住院，他也在百忙中抽时间去看望。校内外来找他请教问题的人很多，他总是耐心地听取别人提出的问题，认真地和别人讨论，把别人的事情完全当成自己的事情去考虑。他担任了多种兼职，可是却从来不考虑报酬。
　　“文化大革命”中受伤的身体使他几次不得不躺在医院的病床上，就是在这种情况下，他仍然看资料，还常常把研究生叫到他的病床前，指导他们的研究工作，为他们批改论文。他的学生怎么能不从心里敬佩、感激这样的导师呢！
　　(作者：杨冶)
简历
　　１９２３年４月１日　生于江西省南昌市。
　　１９４１—１９４５年　重庆中央大学航空工程系学习，获航空工程学士学位。
　　１９４５—１９４７年　任中央大学助教。
　　１９４７—１９４８年　美国明尼苏达大学航空工程系学习，获航空工程硕士学位。
　　１９４８—１９５０年　美国加利福尼亚理工学院航空系学习，获航空数学哲学博士学位。
　　１９５１—１９５２年　任中国科学院数学研究所助理研究员。
　　１９５２—１９７０年　任哈尔滨军事工程学院教授、空气动力学教研室副主任。
　　１９７０年—　任西北工业大学教授、空气动力学研究室主任。
　　１９７８—１９８３年　任西北工业大学副校长。
　　１９８７年—　分别任中国航空学会、中国力学学会、中国空气动力学研究会理事，《航空学报》、《力学学报》编委。
主要论著
１　罗时钧．超音速旋转体与机翼当升力不为零时的波阻力．航空学报，１９６５（３）．
　　２　罗时钧等．跨音速定常势流的混合差分法．北京：国防工业出版社，１９７９．
　　３　ＬｕｏＳ Ｊ．．Ｆｉｎｉｔｅ ｄｉｆｆｅｒｅｎｃｅ ｃｏｍｐｕｔａｔｉｏｎ ｆｏｒ ｔｒａｎｓｏｎｉｃ ｓｔｅａｄｙ ｐｏｔｅｎｔｉａｌ ｆｌｏｗ．Ｃｏｍｐｕｔｅｒ Ｍｅｔｈｏｄｓ ｉｎ Ａｐｐｌｉｅｄ Ｍｅｃｈａｎｉｃｓ ａｎｄ Ｅｎｇ．，１９８１，２７：１２９—３８．
　　４　Ｌｕｏ Ｓ．Ｊ．．Ｓｏｍｅ ｄｉｆｆｅｒｅｎｃｅ ｃｏｍｐｕｔａｔｉｏｎ ｏｆ ｔｒａｎｓｏｎｉｃ ｓｔｅａｄｙ ｓｍａｌｌ ｄｉｓ－ｔｕｒｂａｎｃｅ ｐｏｔｅｎｔｉａｌ ｆｌｏｗ．Ｃｏｌｌ．Ｐａｐｅｒｓ ｏｆ Ｃｈｉｎａ－Ｕ．Ｓ Ｗｏｒｋｓｈｏｐ ｏｎ Ａｄｖ．ｉｎ ＣＯｍｐ．Ｅｎｇ．Ｍｅｃｈ．１９８３．
　　５　Ｌｕｏ Ｓ．Ｊ．．Ｐｏｔｅｎｔｉａｌ ｅｑｕａｔｉｏｎ ｆｏｒ ｔｒａｎｓｏｎｉｃ ｓｔｅａｄｙ ｆｌｏｗ ｗｉｔｈ ｌａｒｇｅ ｌｏｎ－ｇｉｔｕｄｉｎａｌ ｄｉｓｔｕｒｂａｎｃｅ ａｎｄ ｌｉｎｅ ｒｅｌａｘａｔｉｏｎ Ｂｅｉｊｉｎｇ：ＰｒｏＣｅｅｄｉｎｇ ｏｆ Ｓｅｃｏｎｄ Ａｓｉａｎ Ｃｏｎｇｒｅｓｓ ｏｆ Ｆｌｕｉｄ Ｍｅｃｈａｎｉｃｓ，１９８３．
　　６　Ｌｕｏ Ｓ．Ｊ．．ｅｔ．ａｌ．．Ｃｏｍｐｕｔａｔｉｏｎ ｏｆ ｔｒａｎｓｏｎｉｃ ｆｌｏｗ ａｒｏｕｎｄ ａｉｒｆｏｉｌｓ．ｌｓｔ Ｗｏｒｌｄ Ｃｏｎｇｒｅｓｓ ｏｎ Ｃｏｍｐｕｔａｔｉｏｎａｌ Ｍｅｃｈａｎｉｃｓ，Ａｕｓｔｉｎ，ＴＸ，ＵＳＡ：Ｓｅｐ．１９８６，Ｓｅｐｔ．；２２—２６．
　　７　Ｌｕｏ Ｓ．Ｊ．ｅｔ ａｌ．．Ｃｏｍｐｕｔａｔｉｏｎ ｏｆ ｔｒａｎｓｏｎｉｃ ａｅｒｏｄｙｎａｍｉｃａｌｌｙ ｃｏｍｐｅｎｓａｔ－ｉｎｇ ｐｉｔｏｔ ｔｕｂｅ．ＵＳＡ：ＡＩＡＡ ８７—２６１３ｃｐ．
　　８　Ｌｕｏ Ｓ．Ｊ．．Ｃｏｍｐｕｔｅｒ ｓｉｍｕｌａｔｉｏｎ ｏｆ ｌｏｗ　Ｓｐｅｅｄ ｖｏｒｔｉｃａｌ ｆｌｏｗ ａｒｏｕｎｄ ｂｏｄｙ ｏｆ ｒｅｖｏｌｕｔｉｏｎ ａｔ ｈｉｇｈ ａｎｇｌｅｓ ｏｆ ａｔｔａｃｋ．Ｓｈｅｎｚｈｅｎ，Ｃｈｉｎａ：Ｐｒｏｃ．Ｉｎｔｅｒｎ．Ｃｏｎｆ．Ｍｏｄｅｌｌｉｎｇ ＆ Ｓｉｍｕｌａｔｉｏｎ，１９８８，Ｎｏｖｅｍｂｅｒ：７—９．
　　９　Ｐａｉ．Ｓ．Ｉ．Ｌｕｏ Ｓ．Ｊ．．Ｔｈｅｏｒｅｔｉｃａｌ ａｎｄ Ｃｏｍｐｕｔａｔｉｏｎａｌ Ｄｙｎａｍｉｃｓ ｏｆ ａ Ｃｏｍｐｒｅｓｓｉｂｌｅ Ｆｌｏｗ．北京：科学出版社（英文版），１９９０．
　　１０　张武，罗时钧．非对称涡流机理的数值研究．力学学报，１９９０，２２（５）．

看看过去，想想现在，西工大在走下坡路啊！

第一排中间的大胡子老师 长得像爱因斯坦

罗时钧教授　１９７０年—　任西北工业大学教授、空气动力学研究室主任。
１９７８—１９８３年　任西北工业大学副校长。
他培养的博士生蔡晋生是2008年教育部“长江学者”特聘教授。蔡晋生1983年毕业于北京大学力学系，获得理学学士学位。1992年毕业于西北工业大学飞机系，获得工学博士学位。
今天下午在正禾宾馆参加了西北工业大学悼念钱学森追思会，航天学院和航空学院的许多老教授和老院士在座，蔡晋生教授作为钱学森弟子的弟子在场发言

那就是爱因斯坦 那是牛人存在最多的一张照片

听过这么一个牛人，但是没多少人了解

楼主那张照片里就有薛定谔

没错的话 应该是最后一排中间那位高一点的

现在还在做科研的老师，真的好少

西工大这样的泰斗太低调了。我是现在才知道。

西工大还有这样老师没？谁给譬如几个？弟子的弟子还有几分样子？弟子的弟子的弟子都他奶奶啥P样了？

致敬！

学罗老师的跨音速空气动力学，那本小册子写的不错啊，怎么没出书呢

罗老早已远离西工大

今天下午参加学校缅怀钱学森先生追思会时，校长书记还提到罗老 罗老现在美国 没能到场 他的学生发的言 罗老是钱先生的第一个博士弟子 当初追随钱老义无反顾的回国 并因此在日本坐牢三个月 很是佩服

仅仅是不在西工大而已，联系还是很密切的。

永远的罗老师！

罗老师平时不休周末，基本上天天在工作，他今年过年也只休了一周，老人家目前身体很好。很荣幸天天能跟我们罗老爷子聊天。

我一直好奇，西工大为什么对学校历史上出现的这些牛逼闪闪的人从来不做宣传呢？
可以说，这类照片和教授往出来一堆，比金六福搞八年的先进性管用多了啊！