| Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations S Obayashi, GP Guruswamy AIAA journal 33 (6), 1134-1141, 1995 | 378 | 1995 |
| Unsteady aerodynamic and aeroelastic calculations for wings using Euler equations GP Guruswamy AIAA journal 28 (3), 461-469, 1990 | 190 | 1990 |
| A review of numerical fluids/structures interface methods for computations using high-fidelity equations GP Guruswamy Computers & structures 80 (1), 31-41, 2002 | 106 | 2002 |
| Fluid-structural interactions using Navier-Stokes flow equations coupled with shell finite element structures G GURUSWAMY, C Byun 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference, 3087, 1993 | 102 | 1993 |
| A parallel multiblock mesh movement scheme for complex aeroelastic applications M Potsdam, G Guruswamy 39th Aerospace Sciences Meeting and Exhibit, 716, 2001 | 75 | 2001 |
| Aeroelastic time response analysis of thin airfoils by transonic code LTRAN2 P Guruswamy, TY Yang Computers & Fluids 9 (4), 409-425, 1981 | 71 | 1981 |
| A CFD/CSD interaction methodology for aircraft wings M Bhardwaj, R Kapania, E Reichenbach, G Guruswamy 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and …, 1997 | 56 | 1997 |
| Navier-Stokes computations for oscillating control surfaces S Obayashi, GP Guruswamy Journal of aircraft 31 (3), 631-636, 1994 | 56 | 1994 |
| ENSAERO—A multidisciplinary program for fluid/structural interaction studies of aerospace vehicles GP Guruswamy Computing Systems in Engineering 1 (2-4), 237-256, 1990 | 55 | 1990 |
| A Sector Finite Element for Dynamic Analysis of Thick Plates, P. Guruswamy, and T. Y Yang Jl. of Sound and Vibration, Vol. 62, No. 4, February 1979, pp. 505-516 62 (4 …, 1979 | 50* | 1979 |
| Computational fluid dynamics/computational structural dynamics interaction methodology for aircraft wings MK Bhardwaj, RK Kapania, E Reichenbach, GP Guruswamy AIAA journal 36 (12), 2179-2186, 1998 | 49 | 1998 |
| Integrated approach for active coupling of structures and fluids GP Guruswamy AIAA journal 27 (6), 788-793, 1989 | 49 | 1989 |
| Vortical flow computations on swept flexible wings using Navier-Stokes equations GP Guruswamy AIAA journal 28 (12), 2077-2084, 1990 | 48 | 1990 |
| Coupled finite-difference/finite-element approach for wing-body aeroelasticity G GURUSWAMY 4th Symposium on Multidisciplinary Analysis and Optimization, 4680, 1992 | 46 | 1992 |
| Finite element analysis of thick annular and sector plates MN Bapu Rao, P Guruswamy, KS Sampathkumaran Nuclear Engineering and Design; v. 41(2); p. 247-255 41 (2), 247-255, 1977 | 42* | 1977 |
| A parallel, multi-block, moving grid method for aeroelastic applications on full aircraft C Byun, G Guruswamy 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and …, 1998 | 41 | 1998 |
| Direct coupling of Euler flow equations with plate finite element structures GP Guruswamy, C Byun AIAA journal 33 (2), 375-377, 1995 | 39 | 1995 |
| Navier-Stokes computations on swept-tapered wings, including flexibility GP Guruswamy Journal of aircraft 29 (4), 588-597, 1992 | 37 | 1992 |
| Time-accurate unsteady aerodynamic and aeroelastic calculations for wings using Euler equations GP Guruswamy | 37 | 1988 |
| Vortical flow computations on a flexible blended wing-body configuration GP Guruswamy AIAA journal 30 (10), 2497-2503, 1992 | 35 | 1992 |
Shigeru ObayashiInstitute of Fluid Sciecne, Tohoku University在 ifs.tohoku.ac.jp 的电子邮件经过验证
