Books on the topic 'The symplectic Euler method'
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Ta'asan, Shlomo. Canonical-variables multigrid method for steady-state Euler equations. Langley Research Center, 1994.
Find full textSmith, Ralph C. Numerical recovery of material parameters in Euler-Bernoulli beam models. Institute for Computer Applications in Science and Engineering, 1991.
Find full textSmith, Ralph C. A fully Sinc-Galerkin method for Euler-Bernoulli beam models. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1990.
Find full textSmith, Ralph C. A fully Sinc-Galerkin method for Euler-Bernoulli beam models. Institute for Computer Applications in Science and Engineering, 1990.
Find full textCockburn, Bernardo. The Pl-RKDG method for two-dimensional Euler equations of gas dynamics. Institute for Computer Applications in Science and Engineering, 1991.
Find full textRoberts, Thomas W. Solution method for a hovering helicopter rotor using the Euler equations. American Institute of Aeronautics and Astronautics, 1985.
Find full textIollo, Angelo. Pseudo-time method for optimal shape design using the Euler equations. Institute for Computer Applications in Science and Engineering, 1995.
Find full textDang, T. Q. An Euler correction method for two and three-dimensional transonic flows. AIAA, 1987.
Find full textIollo, Angelo. Shape optimization governed by the Euler equations using an adjoint method. Institute for Computer Applications in Science and Engineering, 1993.
Find full textManna, M. A three dimensional high resolution upwind finite volume Euler solver. Von Karman Institute for Fluid Dynamics, 1992.
Find full textPerthame, B. On positivity preserving finite volume schemes for compressible Euler equations. Institute for Computer Applications in Science and Engineering, 1993.
Find full textLee, Dong-Ho. An efficient method to calculate rotor flow in hover & forward flight. American Institute of Aeronautics and Astronautics, 1993.
Find full textShapiro, Richard A. Adaptive finite element solution algorithm for the Euler equations. Vieweg, 1991.
Find full textIollo, Angelo. Shape optimization governed by the Euler equations using an adjoint method [microform]. National Aeronautics and Space Administration, Langley Research Center, 1993.
Find full textCockburn, B. The P¹-RKDG method for two-dimensional Euler equations of gas dynamics. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textBlanco, Max. An implicit solution method for the Euler equations on unstructured triangular grids. National Library of Canada, 1995.
Find full textCockburn, B. The P¹-RKDG method for two-dimensional Euler equations of gas dynamics. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textAnderson, W. Kyle. Grid generation and flow solution method for Euler equations on unstructured grids. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Find full textCockburn, B. The P¹-RKDG method for two-dimensional Euler equations of gas dynamics. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textDeshpande, Suresh M. A second-order accurate kinetic-theory-based method for inviscid compressible flows. Langley Research Center, 1986.
Find full textTurkel, Eli. Accuracy of schemes for the Euler equations with non-uniform meshes. ICASE, 1985.
Find full textLöhner, Rainald. Finite element flux-corrected transport (FEM-FCT) for the Euler and Navier-Stokes equations. ICASE, 1987.
Find full textSchonfeld, Thilo. Methods to enhance the accuracy of finite volume schemes II. Aeronautical Research Institute of Sweden, 1991.
Find full textSmith, Ralph C. A fully Galerkin method for the recovery of stiffness and damping parameters in Euler-Bernoulli beam models. Institute for Computer Applications in Science and Engineering, 1991.
Find full textBonhaus, Daryl L. Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic flight data. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textMatching of orbital integrals on GL(4) and GSp(2). American Mathematical Society, 1999.
Find full textArthur, Rizzi, and Hirschel Ernst-Heinrich, eds. Numerical solutions of the Euler equations for steady flow problems. Vieweg, 1991.
Find full textEberle, Albrecht. Numerical solutions of the Euler equations for steady flow problems. Vieweg, 1992.
Find full textYoon, Seokkwan. An LU-SSOR scheme for the Euler and Navier-Stokes equations. American Institute of Aeronautics and Astronautics, 1987.
Find full textTadmor, Eitan. A minimum entrophy principle in the gas dynamics equations. National Aeronautics and Space Administration, 1986.
Find full textMoitra, Anutosh. Application of a Runge-Kutta scheme for high-speed inviscid internal flows. ICASE, 1986.
Find full textTadmor, Eitan. A minimum entrophy principle in the gas dynamics equations. National Aeronautics and Space Administration, 1986.
Find full textSmith, Ralph C. A fully Galerkin method for the recovery of stiffness and damping parameters in Euler-Bernoulli beam models. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textFelici, Helene M. A coupled Eulerian/Lagrangian method for the solution of three-dimensional vortical flows. National Aeronautics and Space Administration, 1992.
Find full textFelici, Helene M. A coupled Eulerian/Lagrangian method for the solution of three-dimensional vortical flows. Gas Turbine Laboratory, Massachusetts Institute of Technology, 1992.
Find full textBoretti, A. A. Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows. NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.
Find full textBoretti, A. A. Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows. NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.
Find full textBourdel, Francoise. Formulation variationnelle entropique des systemes hyperboliques conservatifs - Application a la resolution des equations d'Euler. Centre d'etudes et de recherches de Toulouse, Departement d'etudes et de recherches en informatique, 1985.
Find full textAtkins, H. L. A multi-block multigrid method for the solution of the Euler and Navier-Stokes equations for three-dimensional flows. American Institute of Aeronautics and Astronautics, 1991.
Find full textCoirier, William J. An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations. National Aeronautics and Space Administration, 1994.
Find full textCanonical-variables multigrid method for steady-state Euler equation. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textCenter, Lewis Research, ed. An efficient method for solving the steady Euler equations. National Aeronautics and Space Administration, Lewis Research Center, 1986.
Find full textCenter, Langley Research, ed. Canonical-variables multigrid method for steady-state Euler equation. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textCanonical-variables multigrid method for steady-state Euler equation. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textWing flutter boundary prediction using an unsteady Euler aerodynamic method. National Aeronautics and Space Administration, Langley Research Center, 1993.
Find full textL, Bowers Kenneth, Lund J, Langley Research Center, and Institute for Computer Applications in Science and Engineering., eds. A fully Sinc-Galerkin method for Euler-Bernoulli beam models. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1990.
Find full textGeojoe, Kuruvila, Ta'asan Shlomo, and Institute for Computer Applications in Science and Engineering., eds. Pseudo-time method for optimal shape design using the Euler equations. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.
Find full textGeojoe, Kuruvila, Ta'asan Shlomo, and Institute for Computer Applications in Science and Engineering., eds. Pseudo-time method for optimal shape design using the Euler equations. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.
Find full textA preconditioning method for shape optimization governed by the Euler equations. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.
Find full textGeojoe, Kuruvila, Ta'asan Shlomo, and Institute for Computer Applications in Science and Engineering., eds. Pseudo-time method for optimal shape design using the Euler equations. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.
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