Libros sobre el tema "Method analysis grids"
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Anderson, W. Kyle. Grid generation and flow solution method for Euler equations on unstructured grids. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Buscar texto completoCarney, Dan. The adjoint method for optimal aerodynamic design on unstructured grids. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.
Buscar texto completoHu, Fang Q. Eigensolution analysis of the discontinuous Galerkin method with non-uniform grids. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2001.
Buscar texto completoT, Tzong y United States. National Aeronautics and Space Administration., eds. A general interface method for aeroelastic analysis of aircraft. [Washington, DC: National Aeronautics and Space Administration, 1996.
Buscar texto completoInstitute for Computer Applications in Science and Engineering., ed. Multigrid method for the equilibrium equations of elasticity using a compact scheme. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1986.
Buscar texto completo1942-, Eiseman Peter R., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. y Langley Research Center, eds. A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Buscar texto completo1942-, Eiseman Peter R., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. y Langley Research Center, eds. A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Buscar texto completoUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. An algebraic homotopy method for generating quasi-three-dimensional grids for high-speed configurations. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Buscar texto completoC, Taylor Arthur, Barnwell Richard W y United States. National Aeronautics and Space Administration., eds. Aerodynamic shape sensitivity analysis and design optimization of complex configurations using unstructured grids. [Washington, DC: National Aeronautics and Space Administration, 1997.
Buscar texto completoHu, Chang-Qing. Weighted essentially non-oscillatory schemes on triangular meshes. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.
Buscar texto completoChi-Wang, Shi y Institute for Computer Applications in Science and Engineering., eds. Weighted essentially non-oscillatory schemes on triangular meshes. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.
Buscar texto completoChi-Wang, Shi y Institute for Computer Applications in Science and Engineering., eds. Weighted essentially non-oscillatory schemes on triangular meshes. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.
Buscar texto completoA, Felippa Carlos, Park K. C y United States. National Aeronautics and Space Administration., eds. Error estimation and adaptive mesh refinement for parallel analysis of shell structures. Boulder, Colo: Dept. of Aerospace Engineering Sciences and Center for Aerospace Structures, University of Colorado, 1994.
Buscar texto completoA, Felippa Carlos, Park K. C y United States. National Aeronautics and Space Administration., eds. Error estimation and adaptive mesh refinement for parallel analysis of shell structures. Boulder, Colo: Dept. of Aerospace Engineering Sciences and Center for Aerospace Structures, University of Colorado, 1994.
Buscar texto completoB, Ransom Jonathan, Aminpour Mohammad A y Langley Research Center, eds. Cross-surface interface element for coupling built-up structural subdomains. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Buscar texto completoB, Ransom J., Aminpour M. A y Langley Research Center, eds. Cross-surface interface element for coupling built-up structural subdomains. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Buscar texto completoB, Ransom Jonathan, Aminpour Mohammad A y Langley Research Center, eds. Cross-surface interface element for coupling built-up structural subdomains. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Buscar texto completoGeorge, Alan. An analysis of spectral envelope-reduction via quadratic assignment problems. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Buscar texto completoGeorge, Alan. An analysis of spectral envelope-reduction via quadratic assignment problems. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Buscar texto completoZhang, Yong-Tao. High order WENO schemes for Hamilton-Jacobi equations on triangular meshes. Hampton, Va: ICASE, NASA Langley Research Center, 2001.
Buscar texto completoC, Hall Kenneth y United States. National Aeronautics and Space Administration., eds. Sensitivity analysis for aeroacoustic and aeroelastic design of turbomachinery blades: Final technical report. Durham, NC: Dept. of Mechanical Engineering and Materials Science, School of Engineering, Duke University, 1995.
Buscar texto completoS, Liou M. y Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. On the application of chimera/unstructured hybrid grids for conjugate heat transfer. Cleveland, Ohio: NASA Lewis Research Center, ICOMP, 1995.
Buscar texto completoMeng-Sing, Liou y Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. On the application of chimera/unstructured hybrid grids for conjugate heat transfer. Cleveland, Ohio: NASA Lewis Research Center, ICOMP, 1995.
Buscar texto completoLewis Research Center. Institute for Computational Mechanics in Propulsion., ed. Calculation of 3D turbulent jets in crossflow with a multigrid method and a second-moment closure model. Cleveland,Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.
Buscar texto completoCenter, Langley Research, ed. A novel shape parameterization approach. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoCenter, Langley Research y United States. National Aeronautics and Space Administration., eds. Euler technology assessment: SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Buscar texto completoRupak, Biswas, Gabow Harold N y Research Institute for Advanced Computer Science (U.S.), eds. Performance analysis and portability of the PLUM load balancing system. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1998.
Buscar texto completoLiseĭkin, V. D. Grid generation methods. Berlin: Springer, 1999.
Buscar texto completoCarey, Graham F. Computational grids: Generation, adaptation, and solution strategies. Washington, D.C: Taylor & Francis, 1997.
Buscar texto completoCenter, Langley Research, ed. Adaptive mesh stategies for the spectral element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Buscar texto completoM, Price John. Adaptive computational methods for aerothermal heating analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Buscar texto completoN, Tiwari S. y United States. National Aeronautics and Space Administration., eds. Investigation of advancing front method for generating front method for generating unstructured grid: Progress report for the period ended May 31, 1991. Norfolk, Va: Old Dominion University Research Foundation, 1992.
Buscar texto completoHesthaven, J. S. High-order/spectral methods on unstructured grids. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2001.
Buscar texto completoI, Warburton y Institute for Computer Applications in Science and Engineering., eds. High-order/spectral methods on unstructured grids. Hampton, VA: ICASE, National Aeronautics and Space Administration, Langley Research Center, 2001.
Buscar texto completoI, Warburton y Institute for Computer Applications in Science and Engineering., eds. High-order/spectral methods on unstructured grids. Hampton, VA: ICASE, National Aeronautics and Space Administration, Langley Research Center, 2001.
Buscar texto completoCenter, Langley Research, ed. Unstructured viscous grid generation by advancing-front method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Buscar texto completoBaden, Scott B. Structured Adaptive Mesh Refinement (SAMR) Grid Methods. New York, NY: Springer New York, 2000.
Buscar texto completoBaysal, Oktay. An overlapped grid method for multigrid, finite volume/difference flow solvers - MaGGiE. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Buscar texto completoNguyen, Hung Lee. On the applications of algebraic grid generation methods based on transfinite interpolation. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Buscar texto completoJameson, Leland M. A wavelet-optimized, very high order adaptive grid and order numerical method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Buscar texto completoMulti-grid methods and applications. Berlin: Springer-Verlag, 1985.
Buscar texto completoZ, Pirzadeh Shahyar y Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Buscar texto completoZ, Pirzadeh Shahyar y Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Buscar texto completoZ, Pirzadeh Shahyar y Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Buscar texto completoZ, Pirzadeh Shahyar y Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Buscar texto completoFrink, Neal T. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Buscar texto completoSigal, Ian Alejandro. Accuracy issues on unstructured grids. Ottawa: National Library of Canada, 2002.
Buscar texto completoSigal, Ian Alejandro. Accuracy issues on unstructured grids. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2002.
Buscar texto completoStanly, Steinberg, ed. Conservative finite-difference methods on general grids. Boca Raton: CRC Press, 1996.
Buscar texto completoWorld Conference on Boundary Elements and Other Mesh Reduction Methods (31st 2009 Wessex Institute of Technology). Mesh reduction methods: BEM/MRM XXXI. Editado por Brebbia C. A. Southampton, UK: WIT, 2009.
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