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Volumn , Issue , 1997, Pages 419-445

An efficient multiblock method for aerodynamic analysis and design on distributed memory systems

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; AERODYNAMICS; COMPLEX NETWORKS; COMPUTATIONAL FLUID DYNAMICS; DESIGN; DISTRIBUTED COMPUTER SYSTEMS; DRAG; FIGHTER AIRCRAFT; FLUID DYNAMICS; MEMORY ARCHITECTURE; MESSAGE PASSING; OPTIMIZATION;

EID: 84983119380     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (54)
  • 2
    • 84983105809 scopus 로고    scopus 로고
    • Satofuka, Periaux, and Ecer, editors, Parallel Computational Fluid Dynamics: New Algorithms and Applications, pages 435-442, Kyoto, Japan, May 1994. Elsevier Science B. V. Parallel CFD ‘94 Conference
    • J. J. Alonso, T. J. Mitty, L. Martinelli, and A. Jameson. A two-dimensional multigrid Navier-Stokes solver for multiprocessor architectures. In Satofuka, Periaux, and Ecer, editors, Parallel Computational Fluid Dynamics: New Algorithms and Applications, pages 435-442, Kyoto, Japan, May 1994. Elsevier Science B. V. Parallel CFD ‘94 Conference.
    • A Two-Dimensional Multigrid Navier-Stokes Solver for Multiprocessor Architectures
    • Alonso, J.J.1    Mitty, T.J.2    Martinelli, L.3    Jameson, A.4
  • 4
    • 0026391155 scopus 로고
    • Aerodynamic sensitivity analysis methods for the compressible Euler equations
    • O. Baysal and M. E. Eleshaky. Aerodynamic sensitivity analysis methods for the compressible Euler equations. Journal of Fluids Engineering, 113(4): 681-688, 1991.
    • (1991) Journal of Fluids Engineering , vol.113 , Issue.4 , pp. 681-688
    • Baysal, O.1    Eleshaky, M.E.2
  • 5
    • 0026833191 scopus 로고
    • Aerodynamic design optimization using sensitivity analysis and computational fluid dynamics
    • O. Baysal and M. E. Eleshaky. Aerodynamic design optimization using sensitivity analysis and computational fluid dynamics. AIAA Journal, 30(3): 718-725, 1992.
    • (1992) AIAA Journal , vol.30 , Issue.3 , pp. 718-725
    • Baysal, O.1    Eleshaky, M.E.2
  • 6
    • 0027553933 scopus 로고
    • Airfoil shape optimization using sensitivity analysis on viscous flow equations
    • O. Baysal and M. E. Eleshaky. Airfoil shape optimization using sensitivity analysis on viscous flow equations. Journal of Fluids Engineering, 115: 75-84, 1993.
    • (1993) Journal of Fluids Engineering , vol.115 , pp. 75-84
    • Baysal, O.1    Eleshaky, M.E.2
  • 7
    • 84983145922 scopus 로고
    • Aerodynamic shape optimization using preconditioned conjugate gradient methods
    • G. W. Burgreen and O. Baysal. Aerodynamic shape optimization using preconditioned conjugate gradient methods. AIAA paper 93-3322, July 1993.
    • (1993) AIAA Paper , pp. 93-3322
    • Burgreen, G.W.1    Baysal, O.2
  • 18
    • 0017995820 scopus 로고
    • Wing design by numerical optimization
    • R. M. Hicks and P. A. Henne. Wing design by numerical optimization. Journal of Aircraft, 15: 407-412, 1978.
    • (1978) Journal of Aircraft , vol.15 , pp. 407-412
    • Hicks, R.M.1    Henne, P.A.2
  • 21
    • 0344047770 scopus 로고
    • Solution of the Euler equations for two dimensional transonic flow by a multigrid method
    • A. Jameson. Solution of the Euler equations for two dimensional transonic flow by a multigrid method. Applied Mathematics and Computations, 13: 327-356, 1983.
    • (1983) Applied Mathematics and Computations , vol.13 , pp. 327-356
    • Jameson, A.1
  • 22
    • 0002992471 scopus 로고
    • Multigrid algorithms for compressible flow calculations
    • W. Hackbusch and U. Trottenberg, editors, Proceedings of the 2nd European Conference on Multigrid Methods, Cologne, 1985, Springer-Verlag
    • A. Jameson. Multigrid algorithms for compressible flow calculations. In W. Hackbusch and U. Trottenberg, editors, Lecture Notes in Mathematics, Vol. 1228, pages 166-201. Proceedings of the 2nd European Conference on Multigrid Methods, Cologne, 1985, Springer-Verlag, 1986.
    • (1986) Lecture Notes in Mathematics , vol.1228 , pp. 166-201
    • Jameson, A.1
  • 23
    • 20544476549 scopus 로고
    • Aerodynamic design via control theory
    • A. Jameson. Aerodynamic design via control theory. Journal of Scientific Computing, 3: 233-260, 1988.
    • (1988) Journal of Scientific Computing , vol.3 , pp. 233-260
    • Jameson, A.1
  • 26
    • 84954695021 scopus 로고
    • Analysis and design of numerical schemes for gas dynamics 1, artificial diffusion, upwind biasing, limiters and their effect on multigrid convergence
    • A. Jameson. Analysis and design of numerical schemes for gas dynamics 1, artificial diffusion, upwind biasing, limiters and their effect on multigrid convergence. Int. J. of Comp. Fluid Dyn., 4: 171-218, 1995.
    • (1995) Int. J. of Comp. Fluid Dyn , vol.4 , pp. 171-218
    • Jameson, A.1
  • 27
    • 84864361143 scopus 로고
    • Analysis and design of numerical schemes for gas dynamics 2, artificial diffusion and discrete shock structure
    • A. Jameson. Analysis and design of numerical schemes for gas dynamics 2, artificial diffusion and discrete shock structure. Int. J. of Comp. Fluid Dyn., 5: 1-38, 1995.
    • (1995) Int. J. of Comp. Fluid Dyn , vol.5 , pp. 1-38
    • Jameson, A.1
  • 28
    • 84983103398 scopus 로고
    • Optimum aerodynamic design using CFD and control theory. AIAA paper 95-1729
    • San Diego, CA
    • A. Jameson. Optimum aerodynamic design using CFD and control theory. AIAA paper 95-1729, AIAA 12th Computational Fluid Dynamics Conference, San Diego, CA, June 1995.
    • (1995) AIAA 12Th Computational Fluid Dynamics Conference
    • Jameson, A.1
  • 33
    • 84983194529 scopus 로고
    • AIAA paper 94~4272, 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City Beach, FL, September
    • A. Jameson and J. Reuther. Control theory based airfoil design using the Euler equations. AIAA paper 94~4272, 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City Beach, FL, September 1994.
    • (1994) Control Theory Based Airfoil Design Using the Euler Equations
    • Jameson, A.1    Reuther, J.2
  • 34
    • 0001097696 scopus 로고
    • Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes
    • A. Jameson, W. Schmidt, and E. Turkel. Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes. AIAA paper 81-1259, January 1981.
    • (1981) AIAA Paper , pp. 81-1259
    • Jameson, A.1    Schmidt, W.2    Turkel, E.3
  • 38
  • 51
    • 0026868040 scopus 로고
    • Subsonic and transonic low-Reynolds-number airfoils with reduced pitching moments
    • J. Reuther, C. P. van Dam, and R. Hicks. Subsonic and transonic low-Reynolds-number airfoils with reduced pitching moments. Journal of Aircraft, 29: 297-298, 1992.
    • (1992) Journal of Aircraft , vol.29 , pp. 297-298
    • Reuther, J.1    Van Dam, C.P.2    Hicks, R.3
  • 53
    • 0004074902 scopus 로고
    • Technical report, Flight Dynamics Laboratory, Wright Research and Development Center, Wright-Patterson Air Force Base, Ohio
    • J. P. Steinbrenner, J. R. Chawner, and C. L. Fouts. The GRIDGEN 3D multiple block grid generation system. Technical report, Flight Dynamics Laboratory, Wright Research and Development Center, Wright-Patterson Air Force Base, Ohio, July 1990.
    • (1990) The GRIDGEN 3D Multiple Block Grid Generation System
    • Steinbrenner, J.P.1    Chawner, J.R.2    Fouts, C.L.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.