About 115 papers listed in the order of date of publication since 1975

Guruswamy, G. P., Anantharama, P.S., and Shah, C.G., "Static Analysis of Low Aspect Ratio Wings by Finite Element Method, '' National Aeronautical Laboratory, India, TM-ST-303-1, April 1975.

Guruswamy, G. P., Shah, C.G., and Somashekar, B.R.," Finite Element Force Method for the Dynamic Analysis of Slender Space Vehicles, '' National Aeronautical Laboratory, India, TM-ST-301-129, April 1976.

Guruswamy, G. P., Kamath, A., and Shah, C.G.," A Computer Procedure for Perspective and Orthographic Plotting of Finite Element Grids, '' National Aeronautical Laboratory, India, TM-ST-301-141, October 1976.

Bapurao, M.N., Guruswamy, G. P., and Sampathkumaran, K.S.," Finite Element Analysis of Thick Annular and Sector Plates, '' International Jl. of Nuclear Engineering and Design, Vol. 41, April 1977, pp. 247-245.

Bapurao, M.N., Guruswamy, G. P., Venkateshwara Rao, M. and Pavithran, S."Studies on Vibration of Some Rib-Stiffened Cantilever Plates,'' International Jl. of Sound and Vibration, Vol. 57, No. 3, April 1978, pp. 389-402.

Yang, T.Y, Striz, A.G. and Guruswamy, G. P. "Flutter Analysis of Two Dimensional and Two Degree of Freedom Airfoils in Small Disturbance Transonic Flow," U S Air Force Flight Dynamics Laboratory, TR-78-202, December 1978.

Guruswamy, G. P. and Yang, T.Y.," A Sector Finite Element for Dynamic Analysis of Thick Plates, ''Jl. of Sound and Vibration, Vol. 62, No. 4 , February 1979, pp. 505-516.

Yang, T.Y. ,Guruswamy, G. P. and Striz, A.G., "Aeroelastic Response Analysis of Two Dimensional, Single and Two Degree of Freedom Airfoils in Low Frequency, Small Disturbance Unsteady Transonic Flow, '' U.S. Air Force Flight Dynamics Laboratory, TR-79-3077, June 1979.

Yang, T.Y., Guruswamy, G. P., and Striz, A.G.,`` Flutter Analysis of a Two Dimensional and Two Degree of Freedom Supercritical Airfoil in Small Disturbance Unsteady Transonic Flow, '' U.S. Air Force Wright Aeronautical Laboratories, TR-80-3010, March 1980.

Yang, T.Y., Guruswamy, G. P., Striz, A.G. and Olsen, J.J.,`` Flutter Analysis of a NACA 64A006 Airfoil in Small Disturbance Transonic Flow, ''Jl. of Aircraft, Vol. 17, No. 4, April 1980, pp. 225-232.

Guruswamy, G. P.," Use of Strained Coordinate Perturbation Method in Transonic Aeroelastic Applications, '' Air Force Wright Aeronautical Laboratories, TR-80-3102, October 1980. Aeronautical Laboratories, TR-80-3102, October 1980. Aeronautical Laboratories, TR-80-3102, October 1980.

Guruswamy, G. P.," Aeroelastic Stability and Time Response Analysis of Conventional and Supercritical Airfoils in Transonic Flow by the Time Integration Method, '' Ph. D. Thesis, Purdue University, December 1980.

Yang, T.Y., Guruswamy, G. P., Striz, A.G. and Olsen, J.J, "Reply by Authors to H.P.Y. Hitch, ''Jl. of Aircraft, Vol. 18, No. 2, February 1981, pp. 159-160.

Yang, T.Y., Striz, A.G., Guruswamy, G. P.," Flutter Analysis of Two Dimensional and Two-Degree-of-Freedom MBB A-3, CAST-7, and TF-8A Supercritical Airfoils in Small Disturbance Unsteady Transonic Flow, '' U S Air Force Wright Aeronautical Laboratories, TR-81-8004, March 1981.

Guruswamy, G. P. and Yang, T. Y.," Aeroelastic Time Response Analysis of Thin Airfoils by Transonic Code LTRAN2, '' Computers and Fluids, Vol. 9, No. 4, Dec. 1981, pp. 409-425.

Yang, T.Y., Guruswamy, G. P., and Striz, A.G., "Application of Transonic Codes to Flutter Analysis of Conventional and Supercritical Airfoils, ''Jl. of Aircraft, Vol. 19, No. 3, March 1982. pp. 211-220.

Guruswamy, G. P. and Goorjian, P. M.," Comparisons Between Computational and Experimental Data in Unsteady Three-Dimensional Transonic Aerodynamics, Including Aeroelastic Applications, '' AIAA Paper No.82-0690-CP, AIAA 23rd Structural Dynamics Conf., New Orleans, May1982 pp. 277-289.

Yang, T.Y., Striz, A.G., and Guruswamy, G. P., "Flutter Analysis of a Two Dimensional and Two Degree of Freedom MBB A-3 Supercritical Airfoil in Two Dimensional Transonic Flow,'' Jl of Aircraft , Vol. 18, No. 10, Oct. 1982, pp. 887-890. (Also AIAA Paper No. 80-0736-CP )

Myers, M. R., Guruswamy, G. P. and Goorjian, P. M.," Flutter Analysis of a Transport Wing Using XTRAN3S , '' AIAA Paper No. 83-0922-CP, AIAA 24th Structural Dynamics Conf., Lake Tahoe, May 1983.

Guruswamy, G. P. and Goorjian, P. M.," Computations and Aeroelastic Applications of Unsteady Transonic Aerodynamics About Wings , '' Jl. of Aircraft, Vol. 21, No. 1, Jan. 1984, pp. 37-43.

Thomas, S. D., Guruswamy, G. P. and Goorjian, P. M.," Use of a Microcomputer for Flutter Analysis of Airfoils, '' 1984 SCS Multiconference., The Society for Computer Simulation, San Diego, CA, Feb. 1984.

(invited) Guruswamy, G. P. and Goorjian, P. M.," Development and Applications of XTRAN3S-Ames (ATRAN3S), '' Computational Fluids Dynamics Users Workshop, The University of Tennessee Space Institute, March 1984.

Guruswamy, G. P. and Goorjian, P. M.," Effects of Viscosity on Transonic Aerodynamic and Aeroelastic Characteristics of Oscillating Airfoils, ''Jpapers.htmll. of Aircraft, Vol. 21, No. 9, Sept. 1984, pp. 700-707. (Also AIAA Paper No. 83-0888-CP , May 1983, pp. 253-265.)

Guruswamy, G. P. and Goorjian, P.M." Efficient Algorithm for Unsteady Transonic Aerodynamics of Low-Aspect-Ratio Wings, '' Jl. of Aircraft ,Vol. 22, No. 3, March 1985, pp. 193-199.

Guruswamy, G. P., Marstiller, J.W, Yang, T.Y, and Goorjian, P.M." Effects of Viscosity and Modes on Transonic Aerodynamic and Aeroelastic Characteristics of Wings, '' Jl. of Aircraft, Vol. 22, No. 9, Sept. 1985, pp. 756-762.

Guruswamy, G. P., Goorjian, P.M. , Merritt, F. J," ATRAN3S : An Unsteady Transonic Code for Clean Wings, '' NASA TM 86783, Dec. 1985.

(invited) Goorjian, P. M. and Guruswamy, G. P. "Unsteady Transonic Aerodynamic and Aeroelastic Calculations about Airfoils and Wings, Paper No. 15, AGARD CP-374, 1984.

(invited) Goorjian, P. M., Guruswamy, G. P., Ide, H., and Miller, G.D, "Transonic Aerodynamic and Aeroelastic Characteristics of a Variable Sweep Wing, '' Paper No. 13, AGARD CP-386, 1985.

Guruswamy, G.P, Goorjian, P.M., Merritt, F.J., " ATRAN3S: An Unsteady Transonic code for Clean Wings, " NASA-TM 86783, Dec 1985

Guruswamy, G. P. "Special Purpose Finite Element Programs, '' Chapter13 of the book Finite Element Structural Analysis, by T.Y. Yang, Prentice-Hall Inc, 1986, pp 481-535.

Guruswamy, G. P. Ide, H. Goorjian, P. M., and Miller, G.D, "Transonic Aeroelastic Analysis of the B-1 Wing, '' Jl. of Aircraft, Vol. 23, No. 7 July 1986, pp 547-553. (also AIAA-85-0690 )

Guruswamy, G. P., Goorjian, P. M. and Tu. E. L., "Unsteady Transonics of a Wing with Tip Store, ''Jl. of Aircraft, Vol. 23, No. 8, August 86. (also AIAA 86-0010 )

Goorjian, P. M. and Guruswamy, G. P., "Transonic Unsteady Aerodynamic and Aeroelastic Calculations about Airfoils and Wings," Jl. of Computers and Structures, Vol. 30, No. 4, pp 929-936, 1988, ( also International Conf. on Computational Engineering Mechanics ICCEM'87, Beijing, China, June, 1987 and also NASA TM 89417)

Goorjian, P. M. and Guruswamy, G. P., "Computational Unsteady Transonic Aerodynamics and Aeroelasticity about Airfoils and Wings,'' International Conf. on Fluid Mechanics ICFM'87, Beijing, China, July 1-4, 1987; also NASA TM 89414, Jan, 1987.

Guruswamy, G. P., Tu, E. L., and Goorjian, P. M., "Transonic Aeroelasticity of Wings with Active Control Surfaces'' AIAA-87-0709, AIAA 28th SDM Conf., Monterey, CA, April 87.

(invited) Guruswamy, G. P. and Goorjian, P. M., "Role of CFD in Unsteady Aerodynamics and Aeroelasticity, '' Symposium on Transonic Unsteady Aerodynamics and Aeroelasticity-1987, Langley Research Center, Hampton, VA, May 1987. (also NASA CP 3022)

Guruswamy, G. P., Goorjian, P. M. and Tu, E. L., "Transonic Aeroelasticity of Wings with Tip Store, ''Jl. of Aircraft, Vol. 24, No. 10, Oct. 1987, pp 688-695. (also Paper No. 86-1007-CP, AIAA 27th Structural Dynamics and Materials Conf., San Antonio, Texas May 1986.)

Guruswamy, G. P. and Goorjian, P. M., "Unsteady Transonic Flow Simulation on a Full-Span Wing-Body Configuration,'', AIAA Jl., Vol. 26, No. 12 Dec. 1988, pp 1450-1456. (also AIAA-87-1240 )

(invited) Guruswamy, G. P., "Interaction of Fluids and Structures for Aircraft Applications, ''Jl. of Computers and Structures ,Vol. 30, No.1/2, pp 1-13, 1988, (also a chapter in book Computational Structural Mechanics and Fluid Dynamics, Advances and Trends, Pergamon Press, Oxford. )

Guruswamy, G. P. and Goorjian, P. M.,"Unsteady Transonic Aerodynamics and Aeroelastic Calculations at Low-Supersonic Freestreams, '' Jl. of Aircraft, Vol. 25, No. 10, Oct 1988.

Guruswamy, G. P." Numerical Simulation of Vortical Flows on Flexible Wings, '' AIAA-89-0537, 27th Aerospace Sciences Meeting, Reno, NE, Jan. 1989.

Guruswamy, G. P. and Tu, E. L., "Effects of Modal Symmetry Aeroelastic Characteristics of Full-Span Wing-Body Configurations, ''Jl. of Aircraft, Vol. 26, No. 3, Mar. 1989, pp 271-280. (also AIAA-88-2308 )

Guruswamy, G. P. "An Integrated Approach for Active Coupling of Structures and Fluids,'' AIAA Jl., Vol. 27, No. 6, June 89, pp 788-793.

43 Guruswamy, G. P. and Tu, E. L., "Transonic Aeroelasticity of Fighter Wings with Active Control Surface, ''Jl. of Aircraft, Vol 26, No. 7, July 1989, pp 682-684.

Guruswamy, G. P. "Unsteady Aerodynamic and Aeroelastic Calculations for Wings Using Euler Equations ''AIAA Jl., Vol. 28, No. 3, March 1990, pp 461-469. (also AIAA Paper 88-2281)

Obayashi, S., Goorjian P. M., and Guruswamy, G. P., "Extension of a Streamwise Upwind Algorithm to a Moving Grid System , '' NASA TM 102800, April 1990.

Obayashi, S., Guruswamy, G. P., and Goorjian P. M." Streamwise Upwind Algorithm for Computing Unsteady Transonic Flows Past Oscillating Wings, ''AIAA Jl., Vol. 29, No. 10, October 1991, pp 1668-1677. ( Also AIAA-90-3103, 8th Applied Aerodynamics Conference, August 1990)

(invited) Guruswamy, G. P., "ENSAERO- A Multidisciplinary Program for Fluid/Structural Interaction Studies of Aerospace Vehicles, '' Computing Systems in Engineering , Vol. 1, No.2- 4, 90, pp 237-256.

Guruswamy, G. P., "Vortical Flow Computations on Swept Flexible Wings Using Navier-Stokes Equations, ''AIAA Jl. , Vol. 28, No. 12, Dec 1990, pp. 2077-2133. (also AIAA-89-1183)

Obayashi, S. and Guruswamy, G. P., "Unsteady Shock-Vortex Interaction on a Flexible Delta Wing,'' Jl of Aircraft, Vol 29, No 5, Sept-Oct 92, pp 790-798. (also AIAA-91-1109-CP, April 1991, 4th International Symposium on CFD, UC Davis, Sept 91.)

Obayashi, S., Guruswamy, G. P. and Tu, E. L., "Unsteady Navier-Stokes Computations on a Wing-Body Configuration in Ramp Motions, '' AIAA-91-2865-CP, August 1991, pp 167-176.

Guruswamy, G. (invited)"Computation of Aeroelasticity Associated With Transonic Vortical and Separated Flows Using ENSAERO, '' HTP- 5 Workshop on Vortical Flow Breakdown and Structural Interactions, NASA Langley Research Center, August 15-16, 1991, Hampton VA.

Guruswamy, G. (invited)"Transonic Aeroelastic Computations on Wings Using Navier-Stokes Equations, '' Paper-22, Conference proceeding on Transonic Unsteady Aerodynamics and Aeroelasticity, AGARD 507, San Diego, 9-11 October 1991.

Goorjian, P. M, Obayashi, S., Chaderjian N. M., and Guruswamy, G. P. "Algorithm Development With Applications To Aerodynamics and Aeroelasticity, '' Lecture Series 1991-1992, No. 6 von Karman Institute for Fluid Dynamics, March 1992.

Chaderjian, N. M. and Guruswamy, G. P. "Transonic Navier-Stokes Computations for an Oscillating Wing Using Zonal Grids, '' Jl. of Aircraft, Vol. 29, No. 3, May-June 1992, pp 326-335. (also AIAA 90-0313, Aerospace Sciences Meeting, Jan. 1990.)

Guruswamy, G.-Stokes Computations on Swept-Tapered Wings, Including Flexibility, '' Jl. of Aircraft, Vol. 29, No. 4, July-August 1992, pp 588-597.(also AIAA-90-1152-CP, AIAA 31st Structural Dynamics Conf., Long Beach, California, April 1990. )

Rizk, Y., Guruswamy, G. and Gee, K. " Numerical Investigation of Tail Buffet of F-18 Aircraft, '' AIAA-92-2673, AIAA 10th Applied Aerodynamics Conference, June 22-24, 1992, Palo Alto, CA.

Guruswamy, G., Weeratunga, S. and Pramono, E. "Direct Coupling Approach to Fluid/Structures Interaction Problems for Parallel Computing , '' Computational Aerosciences Conference, August 18-19, 1992, Ames Research Center Moffett Field, CA.

Obayashi, S. and Guruswamy, G. P., "Navier-Stokes Computations for Oscillating Control Surfaces, '' Jl of Aircraft, Vol 31, No 3, May-June 94 pp 631-636. (also AIAA-92-4431, AIAA Atmospheric Flight Mechanics Conference, August 10-12, 1992, Hilton Head Island, SC.

MacMurdy, D, Kapania, R. and Guruswamy, G. "Aeroelasticity of Wings Using Navier-Stokes Equations Coupled with Wing-Box Finite- Element Structures,'' Computational Aerosciences Conference, August 18-19, 1992, Ames Research Center Moffett Field, CA. (also AIAA- 92-4795, 4th AIAA/USAF/NASA/OAI Symposium on Multidisciplinary Analysis and Optimization, Sept92, Cleveland, OH.)

Guruswamy, G. P., "Coupled Finite-Difference/Finite-Element Approach for Wing-Body Aeroelasticity, '' AIAA 92-4680, 4th AIAA/USAF/NASA/OAI Symposium on Multidisciplinary Analysis and Optimization, September 21-23, 1992, Cleveland, Ohio.

Guruswamy, G. P., "Vortical Flow Computations on a Flexible Blended Wing-Body Configuration, '' AIAA Jl, Vol. 30, No. 10, October 1992. pp 2497-2503, (also AIAA-91-1013-CP, April 1991, pp 719-734 and an invited talk at the 11th Australasian Fluid Mechanics Conf. Hobart, Australia, Dec 1992)

Guruswamy, G. P. and Byun C.," Fluid-Structural Interactions Using Navier-Stokes Flow Equations with Shell Finite-element Structures,'' AIAA-93-3087, 24th Fluid Dynamics Conference, Orlando FL, July 1993.

Tu, E., Obayashi, S., and Guruswamy, G. P." Unsteady Navier-Stokes Simulation of the Canard-Wing-Body-Configuration, '' AIAA-93- 3058, 24th Fluid Dynamics Conference, Orlando FL, July 1993. 09

Byun, C. and Guruswamy, G. P.,"A Comparative Study of Serial and Parallel Aeroelastic Computations, '' Second U.S. National Congress on Computational Mechanics, August 16-18, 1993. (Also NASA TM 108805)

Guruswamy, G. P. and Tu E. ,"Navier-Stokes Computations on Flexible Advanced Transport Wings in Transonic Regime ,'' AIAA 94-1725, Dynamic Specialist Conf, Hilton Head, South Carolina, April 1994.

MacMurdy, D., Guruswamy, G. P. and Kapania, R., "Aeroelastic Analysis of Wings Using Euler/Navier-Stokes Equations Coupled with Improved Wing-Box Finite Element Structures ,'' AIAA 94- 1587, AIAA SDM Conf, Hilton Head, South Carolina, April 1994.

Guruswamy, G. P' User's Guide for ENSAERO- A Multidisciplinary Program for Fluid/Structural/Control Interaction Studies of Aircraft, " NASA TM 108853, Oct. 1994.

Guruswamy, G. P. and Byun, C., "Direct Coupling of the Euler Flow Equations with Plate Finite Element Structures,'' AIAA Jl, Vol 33, No 2, Feb 1995.

Guruswamy, G. P. and Byun, C., "Progress in Computational Aeroelasticity Using High Fidelity Flow and Structural Equations on Parallel Computers", NASA-Computational Aerosciences Workshop- 95, Ames Research Center, Moffett Field, March 1995

Guruswamy, G.P. and Tu, E. "Euler/Navier-Stokes Flow Computations on Flexible Congigurations for Stability Analysis," AIAA 95-1292 36th AIAA Structural Dynamics Conf, April 95

Bhardwaj, M., Byun, C., Kapania, R. and Guruswamy, G.P., "Parallel Aeroelastic Computations by Using Coupled Euler Flow and Wing-Box Equations," AIAA-95-1291, 36th AIAA Structural Dynamics Conf, April 95

Byun, C. and Guruswamy, G. P., "An Efficient Procedure for Flutter Boundary Prediction on Parallel Computer, " AIAA-95-1484, 36th AIAA Structural Dynamics Conf, April 95

Obayashi, S. and Guruswamy, G. P." Convergence Acceleration of a Navier-Stokes Solver for Efficient Static Aeroelastic Computations,'' AIAA Jl, Vol 33, No. 6, June 95, pp 1134-1141. ( also AIAA-94-2268, 25th AIAA Fluid Dynamics Conf, Colorado Springs, CO, June, 94.)

Obayashi, S., Chiu, I., and Guruswamy, G. P." Navier-Stokes Computations on Full-Span Wing-Body Configuration with Oscillating Control Surfaces,'' AIAA JL, Vol 32, No 6, Nov-Dec 95, pp 1227- 1233. (Also AIAA-93-3687, AIAA Atmospheric Flight Mechanics Conference, Monterey, August 9-11, 1993)

Byun, C. and Guruswamy, G. P., "Wing-Body Aeroelasticity on Parallel Computers, '' Jl of Aircraft, Vol 33, No 2, Mar-April 96, pp 421- 428. (Also AIAA 94-1487, Structural Dynamics Conference, Hilton Head, South Carolina, April 1994.)

Farhangnia, M. Guruswamy, G.P. and Biringen, S. "Transonic-Buffet Associated Aeroelasticity of a Supercritical Wing, " AIAA 96-0286, 34th Aerospace Sciences Meeting and Exhibit, Reno NV, Jan 1996.

Byun, C. and Guruswamy, G. P., "Aeroelastic Computations on Wing- Body-Control Configurations on Parallel computers, '' AIAA 96-1389, Structural Dynamics Conference, Salt Lake City, UT , April 1996.

Appa, K, Argyris J.H and Guruswamy G. P., "Aircraft Dynamics and Loads Computations Using CFD Methods, " AIAA 96-1342, Structural Dynamics Conference, Salt Lake City, UT , April 1996.

Guruswamy, P. (invited) " Progress in Integrated Fluid/Structure/Control Computations using High Fidelity Equations "15th International Conference on Numerical Methods in Fluid Dynamics , Monterey, CA, June 24-28, 1996.

Guruswamy, P. " Advances in Fluid/Structures/Controls Computations Using High Fidelity Equations on Serial and Parallel Computers, " 97 Computational Aeroscience Conf, Ames Research Center, Aug 96.

Byun, C and Guruswamy G. P. Static Aeroelasticity Computations for Flexible Wing-Body-Control Configurations, "AIAA-96-4059, 6th AIAA/NASA/USAF MDO Symposium, Sept 1996

Appa, K, Argyris J.H, Guruswamy G. P., Martin ,C.A. "Synergistic Aircraft Design Using CFD Air Loads, " AIAA-96-4057, 6th AIAA/NASA/USAF MDO Symposium, Sept 1996

Kapania, R., Bhardwaj, M. Reichenbach, E, Guruswamy, G.P, " Aeroelastic Analysis of Modren Complex Wings, "AIAA-96-4010 , 6th AIAA/NASA/USAF MDO Symposium, Sept 1996

(invited talk) Guruswamy, G.P. " Progress in Integrated Fluid/Structure/Controls Aeroelastic Computations Using High Fidelity Equations, "Recent Advances in Structural Dynamics and Aeroelasticity, Proceedings of Seventh International Seminar on Aerospace Structures, Bangalore, India Aug 97.

Byun C. and Guruswamy, G. P. " Aeroelastic Computations on Wing- Body-Control Configurations on Parallel Computers, " Jl of Aircraft, Vol 35, No 2 March-April 1998 pp 288-294.

Ferhat H., Jespersen, D., Guruswamy, G.P., Rizk, Y., Byun, C., and Ken G., "A Multi-level Parallelization Concept for High-Fidelity Multi-Block Solvers, " Super Computing 97, San Jose, Nov 1997.

Eldred, L.B., Byun C. and Guruswamy, G. P. " Integration of High Fidelity Analysis into Parallel Multidisciplinary Aircraft Structural Dynamics and Materiels Conf, Long Beach CA, April 1998

Farhangnia, M., Guruswamy, G.P. and Byun, C, " Performance and Applications of ENSAERO_MPI on Scalable Computers, " HPCCP/CAS Workshop 98, Ames Research Center, Moffett Field, CA, August 98

Eldred, L. , Guruswamy, G.P. and Byun, C, " Parallel Aeroelastic Analysis Using ENSAERO and NASTRAN, " HPCCP/CAS Workshop 98, Ames Research Center, Moffett Field, CA, August 98.

Guruswamy, G.P. "Impact of Parallel Computing on High Fidelity Based Multidisciplinary Analysis, " AIAA-98-4709, 7th AIAA/USAF/ NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, St. Louis, MO, Sept 98.

Byun, C and Guruswamy, G.P. "A Parallel Multi-Block Moving Grid Method for Aeroelastic Applications on Full Aircraft"AIAA-98-4782, 7th AIAA/USAF/ NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, St. Louis, MO, Sept 98.

Bhardwaj, M., Kapania, R., Reichenbach and Guruswamy, G.P., " Computational Fluid Dynamics/Computational Structural Dynamics Interaction Methodology for Aircraft Wings, "AIAA Jl Vol 36, No 12, Dec 1998, pp 2179-2186. (Also AIAA-98-4783, 7tt AIAA/USAF/ NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, St. Louis, MO, Sept 98)

Farhangnia, M., Guruswamy, G.P. and Byun, C, " Performance and Applications of ENSAERO_MPI on Scalable Computers, "NASA Ames Research Center, HPCCP/CAS Workshop 98, NASA/CP-1999-208757 Jan 1999.

Eldred, L. , Guruswamy, G.P. and Byun, C, " Parallel Aeroelastic Analysis Using ENSAERO and NASTRAN, "NASA Ames Research Center HPCCP/CAS Workshop 98, NASA/CP-1999-208757, Jan 1999.

Garcia, J A and Guruswamy, G.P. , " Static Aeroelastic Characteristics of an Advanced Wing with a Control Surface Using Navier-Stokes Equations, "AIAA-99-0796, 37th Aerospace Sciences Meeting, Reno NV, Jan 11-14, 99.

Garcia, J A and Guruswamy, G.P. , " Aeroelastic Analysi of Transonic Wings Using Navier-Stokes Equations and a Nonlinear Beam Model, " AIAA 99-1215, 40th SDM Conf St Louis MO, April 99.

Eldred, L. and Guruswamy, G.P., " User's Guide for ENSAERO_FE Parallel Finite Element Solver. NASA TM 1999-208781, April 1999.

Guruswamy, G.P., Byun, C., Farhangnia, M and Potsdam, M. " User's Manual for HiMAP : A Portable 3-Level Parallel Multidisciplinary Analysis Process, " NASA/TM - 1999 -209578, Sept 99.

Byun, C., Farhangnia, M., Guruswamy, G. P., "Aerodynamic Influence Coefficient Computations Using Euler/Navier-Stokes Equations on Parallel Computers, " AIAA Jl, Nov 1999, Vol 37, No 11, pp. 1393-1400 (also AIAA-97- 1086 with Kumar Bhatia, AIAA/ASME/ASCE ASC 38th Structures, Structural Dynamics and Materials Conf, , Kissmmee FL April 97)

Guruswamy, G.P. " HiMAP : A Portable Super Modular Multilevel Parallel Multidisciplinary Process For Large Scale Analysis, " Advances in Engineering Software 31 (2000) 617-620 , Elsevier Oct 2000 (Also invited talk at 5th NASA Symposium Intelligent Synthesis Environment Industry/Academia Workshop, NASA Langley Research Center Oct 28-29, 1999).

Guruswamy, G.P, Potsdam, M and Rodriguez, D , " Applications of Parallel Process HiMAP for Large Scale Multidisciplinary Problems, " Super Computing 2000, Dallas Texas, Nov 2000.

(invited)Guruswamy, G. P " Impact of Parallel Computing on Large Scale Aeroelastic Computations " IEEE/ACM 7th International Conference on High Performance Computing, Bangalore India, Dec 2000.

Potsdam, M.A. and Guruswamy G.P , " A Parallel Multiblock Mesh Movement Scheme for Complex Aeroelastic Applications, " AIAA 2001-0716, 39th AIAA Aerospace Sciences Meeting, Reno Jan 8-11, 2001.

Guruswamy, G.P. " A Review of Numerical Fluids/Structures Interface Methods for Computations using High Fidelity Equations, " Computers and Fluids, (80) (2002)31-41 (Also NASA/TM-2000-209596, October 2000).

Jones , K, Platzer, M., Rodriguez, D. and Guruswamy, G. P. , " On the Effect of Area Ruling on Transonic Abrupt Wing Stall" Symposium Transsonicum IV, Gottingen, Sept 2002.

Guruswamy, G. P., " Development and Applications of a Modular Parallel Process for Large Scale Fluid/Structures Problems, " HPC Asia-2002, Bangalore Dec 2002

Guruswamy, G. P. and Cheung, C. "2D Static Fluid/Structure Analysis Using TCL/Tk Based PSE., " The 2003 International Conference on Parallel and Distyributed Computing, Las Vegas, NV, June 2003.

Guruswamy, G.P " A New Modular Approach for Tightly Coupled Fluid/Structure Analysis," AIAA 2004-4547, 10th AIAA MDO Conference, Albany NY, April 2004.

Guruswamy G.P, "AIC Computations Using Navier-Stokes Equations on Single-Image Supercomputers for Design-Optimization " AIAA-2005-1983 to be presented at SDM meeting April 05.

Guruswamy, G.P. " Computation of High Fidelity Aeroelastic Response Surfaces for Spacecraft on Cluster Supercomputers, " AIAA-2005-1983, 46th AIAA Structural Dynamics Conference, Austin Texas, April 2005.

Striz, A, Byun C, and Guruswamy, G.P, " High Fidelity Dynamic Analysis of Launch Vehicles on Single Image Supercomputers, " AIAA-2005-1940, AIAA Structural Dynamics Conference, Austin Texas April 2005.

Guruswamy, G.P, "Development and Applications of a Large Scale Fluids/Structures Simulation Process on Clusters, " Computers & Fluids 36 (2007) 530-539, March 2007.

Guruswamy, G.P.,"Euler/Navier-Stokes-Based Unsteady Aerodynamics and Aeroelasticity of a Capsule Landing System, " AIAA-2007-2063, 48th AIAA Structural Dynamics Conference, Honolulu, Hawaii, April 2007.

Guruswamy, G.P,"A Modular Approach to Euler/Navier-Stokes-Based Aeroelasticity of Helicopter Rotor Blades, "AIAA-2008-2179,49th AIAA/AHS Structural Dynamics Conf, Chicago, April 2008.

Guruswamy, G.P, "Role of HPC in Advancing Computational Aeroelasticity", Invited Talk at the International Conference on Aerospace Science and Technology, National Aerospace Laboratories, June 2008.