Biography

Prof. Ramesh K. Agarwal

Washington University in St. Louis, USA

Professor


Email: rka@wustl.edu


Qualifications

1975 Ph.D., Stanford University, Aeronautical Sciences

1969 M.Sc., University of Minnesota, Aeronautical Engineering

1968 B.Sc., Indian Institute of Technology, Mechanical Engineering


Publications (Selected)

  1. R. K. Agarwal, “Computational Fluid Dynamics of Whole-Body Aircraft,” Annual Review of Fluid Mechanics, Vol. 31, 1999, pp. 125-169.
  2. R. K. Agarwal and J. E. Deese, “Navier-Stokes Calculations of the Flowfield of a Complete Aircraft,” Advances in Computational Fluid Dynamics, W. G. Habashi, Ed., Springer-Verlag, 1990.
  3. R. K. Agarwal and J. E. Deese, “Navier-Stokes Calculations of Transonic Viscous Flow about Wing-Body Configurations,” Journal of Aircraft, Vol. 25, 1988, pp. 1106-1112.
  4. R. K. Agarwal and J. E. Deese, “Euler/Navier-Stokes Computation of the Flowfield of a Helicopter Rotor in Hover and Forward Flight,” Progress in Aeronautics, P. A. Henne, ed., Vol. 125, AIAA, 1990, pp. 533-555.
  5. R. K. Agarwal and J. E. Deese, “Euler Calculations for the Flowfield of a Helicopter Rotor in Hover,” Journal of Aircraft, Vol. 24, 1987, pp. 231-238.
  6. R. K. Agarwal, T.P. Gielda and T. M. Walters, “Single-Stage to-Orbit (SSTO) Propulsion Installed Performance Predictions and Test,” International Journal of Computational Fluid Mechanics, Vol. 2, 1994, pp. 85-110.
  7. J. E. Deese and R. K. Agarwal, “Turbulent Flow Calculations Over Wings Near Maximum Lift,” Journal of Aircraft, Vol. 27, 1990, pp. 929-935.
  8. R. K. Agarwal and J. E. Deese, “Euler Solutions for Airfoil/Jet/Ground-Interaction Flowfields,” Journal of Aircraft, Vol. 23, 1986, pp. 376-383.
  9. R. K. Agarwal, “Recent Advances in V/STOL Aerodynamics,” Recent Advances in Aerodynamics, A. Krothapalli and C. A. Smith, Eds., Springer-Verlag, 1986, pp. 471-524.
  10. R. K. Agarwal and J. E. Deese, “Recent Advances in Computational Aerodynamics,” Computer Physics Communications, Vol. 65, 1991, pp. 8-16.
  11. R. K. Agarwal, “An Overview of Large Scale Aerospace Applications of CFD,” in Solution Techniques for Large CFD Problems, W. G. Habashi, Ed., John Wiley, 1995, pp. 375-390.
  12. R. K. Agarwal and J. C. Lewis, “Computational Fluid Dynamics on Parallel Processors,” Computing Systems in Engineering, Vol. 3, 1992, pp. 251-259.
  13. R. K. Agarwal “Advanced Computational Technology for Product Design.” in solving Large Scale Problems in Mechanics: Parallel and Distributed Computer Applications, M. Papadrakakis, ed., John Wiley, 1996, pp. 399-433.
  14. D. L. Marcum and R. K. Agarwal, “Finite Element Navier-Stokes Solver for Unstructured Grids,” AIAA Journal, Vol. 30, No. 3, 1992, p. 648.
  15. R. K. Agarwal, K. Yun, and R. Balakrishnan, “Beyond Navier-Stokes: Burnett Equations for Simulation of Transitional Flows,” Physics of Fluids, Vol. 13, Oct. 2001, pp. 3061-3085.
  16. K.Yun and R. K. Agarwal, “Numerical Solution of 3-D Augmented Burnett Equations for Hypersonic Flow in Continuum-Transition Regime,” Journal of Thermophysics and Heat Transfer, Vol. 38, 2001.
  17. J. Cui and R. K. Agarwal, “Three-Dimensional Computation of a Synthetic Jet in Quiescent Flow,” AIAA J., Vol. 44, No. 12, 2006, pp. 2846-2855.
  18. R. K. Agarwal, J. Vadillo, Y.Tan, J. Cui, D. Guo, H. Jain, A.W. Cary and W.W. Bower, “Flow Control with Synthetic and Pulsed Jets: Applications to Virtual Aeroshaping, Thrust-Vectoring, and Control of Separation and Cavity Oscillations,” in Frontiers of Computational Fluid Dynamics , Chapter 11, D.A. Caughey and M. Hafez Editors, World Scientific, NJ, 2006.
  19. R. K. Agarwal and J. Augustinus, “A Characteristics Based Box Scheme for Compressible Eight-Wave Structure Ideal MHD Equations,” Computational Fluid Dynamics Journal, Vol.8, No. 2, July 1999, pp. 170-177.
  20. R. K. Agarwal, K. S. Huh and M. Shu, “A CFD-Based Approach for the Solution of Acoustics, Maxwell, and Schrodinger Equations for Scattering Problems,” Lecture Notes in Physics, M. Napolitano and F. Sabetta, eds., Springer-Verlag, 1993, p. 370-375.


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