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)
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R. K.
Agarwal, “Computational Fluid Dynamics of Whole-Body Aircraft,” Annual Review
of Fluid Mechanics, Vol. 31, 1999, pp. 125-169.
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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.
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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.
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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.
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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.
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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.
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J. E.
Deese and R. K. Agarwal, “Turbulent Flow Calculations Over Wings Near Maximum
Lift,” Journal of Aircraft, Vol. 27, 1990, pp. 929-935.
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R. K.
Agarwal and J. E. Deese, “Euler Solutions for Airfoil/Jet/Ground-Interaction
Flowfields,” Journal of Aircraft, Vol. 23, 1986, pp. 376-383.
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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.
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R. K.
Agarwal and J. E. Deese, “Recent Advances in Computational Aerodynamics,”
Computer Physics Communications, Vol. 65, 1991, pp. 8-16.
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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.
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R. K.
Agarwal and J. C. Lewis, “Computational Fluid Dynamics on Parallel Processors,”
Computing Systems in Engineering, Vol. 3, 1992, pp. 251-259.
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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.
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D. L.
Marcum and R. K. Agarwal, “Finite Element Navier-Stokes Solver for Unstructured
Grids,” AIAA Journal, Vol. 30, No. 3, 1992, p. 648.
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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.
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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.
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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.
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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.
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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.
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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.