Książki na temat „Method analysis grids”

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.

Carney, Dan. The adjoint method for optimal aerodynamic design on unstructured grids. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.

Hu, 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.

T, Tzong, i United States. National Aeronautics and Space Administration., red. A general interface method for aeroelastic analysis of aircraft. [Washington, DC: National Aeronautics and Space Administration, 1996.

Institute for Computer Applications in Science and Engineering., red. 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.

1942-, Eiseman Peter R., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. i Langley Research Center, red. 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.

1942-, Eiseman Peter R., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. i Langley Research Center, red. 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.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

C, Taylor Arthur, Barnwell Richard W i United States. National Aeronautics and Space Administration., red. Aerodynamic shape sensitivity analysis and design optimization of complex configurations using unstructured grids. [Washington, DC: National Aeronautics and Space Administration, 1997.

Hu, 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.

Chi-Wang, Shi, i Institute for Computer Applications in Science and Engineering., red. Weighted essentially non-oscillatory schemes on triangular meshes. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

Chi-Wang, Shi, i Institute for Computer Applications in Science and Engineering., red. Weighted essentially non-oscillatory schemes on triangular meshes. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

A, Felippa Carlos, Park K. C i United States. National Aeronautics and Space Administration., red. 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.

A, Felippa Carlos, Park K. C i United States. National Aeronautics and Space Administration., red. 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.

B, Ransom Jonathan, Aminpour Mohammad A i Langley Research Center, red. Cross-surface interface element for coupling built-up structural subdomains. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

B, Ransom J., Aminpour M. A i Langley Research Center, red. Cross-surface interface element for coupling built-up structural subdomains. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

B, Ransom Jonathan, Aminpour Mohammad A i Langley Research Center, red. Cross-surface interface element for coupling built-up structural subdomains. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

George, 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.

George, 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.

Zhang, Yong-Tao. High order WENO schemes for Hamilton-Jacobi equations on triangular meshes. Hampton, Va: ICASE, NASA Langley Research Center, 2001.

C, Hall Kenneth, i United States. National Aeronautics and Space Administration., red. 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.

S, Liou M., i Lewis Research Center. Institute for Computational Mechanics in Propulsion., red. On the application of chimera/unstructured hybrid grids for conjugate heat transfer. Cleveland, Ohio: NASA Lewis Research Center, ICOMP, 1995.

Meng-Sing, Liou, i Lewis Research Center. Institute for Computational Mechanics in Propulsion., red. On the application of chimera/unstructured hybrid grids for conjugate heat transfer. Cleveland, Ohio: NASA Lewis Research Center, ICOMP, 1995.

Lewis Research Center. Institute for Computational Mechanics in Propulsion., red. 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.

Center, Langley Research, red. A novel shape parameterization approach. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Center, Langley Research, i United States. National Aeronautics and Space Administration., red. 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.

Rupak, Biswas, Gabow Harold N i Research Institute for Advanced Computer Science (U.S.), red. Performance analysis and portability of the PLUM load balancing system. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1998.

Liseĭkin, V. D. Grid generation methods. Berlin: Springer, 1999.

Carey, Graham F. Computational grids: Generation, adaptation, and solution strategies. Washington, D.C: Taylor & Francis, 1997.

Center, Langley Research, red. Adaptive mesh stategies for the spectral element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

M, Price John. Adaptive computational methods for aerothermal heating analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

N, Tiwari S., i United States. National Aeronautics and Space Administration., red. 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.

Hesthaven, J. S. High-order/spectral methods on unstructured grids. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2001.

I, Warburton, i Institute for Computer Applications in Science and Engineering., red. High-order/spectral methods on unstructured grids. Hampton, VA: ICASE, National Aeronautics and Space Administration, Langley Research Center, 2001.

I, Warburton, i Institute for Computer Applications in Science and Engineering., red. High-order/spectral methods on unstructured grids. Hampton, VA: ICASE, National Aeronautics and Space Administration, Langley Research Center, 2001.

Center, Langley Research, red. Unstructured viscous grid generation by advancing-front method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Baden, Scott B. Structured Adaptive Mesh Refinement (SAMR) Grid Methods. New York, NY: Springer New York, 2000.

Baysal, Oktay. An overlapped grid method for multigrid, finite volume/difference flow solvers - MaGGiE. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Nguyen, Hung Lee. On the applications of algebraic grid generation methods based on transfinite interpolation. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Jameson, 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.

Multi-grid methods and applications. Berlin: Springer-Verlag, 1985.

Z, Pirzadeh Shahyar, i Langley Research Center, red. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Z, Pirzadeh Shahyar, i Langley Research Center, red. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Z, Pirzadeh Shahyar, i Langley Research Center, red. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Z, Pirzadeh Shahyar, i Langley Research Center, red. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Frink, 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.

Sigal, Ian Alejandro. Accuracy issues on unstructured grids. Ottawa: National Library of Canada, 2002.

Sigal, Ian Alejandro. Accuracy issues on unstructured grids. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2002.

Stanly, Steinberg, red. Conservative finite-difference methods on general grids. Boca Raton: CRC Press, 1996.

World Conference on Boundary Elements and Other Mesh Reduction Methods (31st 2009 Wessex Institute of Technology). Mesh reduction methods: BEM/MRM XXXI. Redaktor Brebbia C. A. Southampton, UK: WIT, 2009.