Книги з теми "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.
Знайти повний текст джерелаCarney, Dan. The adjoint method for optimal aerodynamic design on unstructured grids. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.
Знайти повний текст джерелаHu, 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.
Знайти повний текст джерелаT, Tzong, and 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.
Знайти повний текст джерелаInstitute 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.
Знайти повний текст джерела1942-, Eiseman Peter R., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., and 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.
Знайти повний текст джерела1942-, Eiseman Peter R., United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., and 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаC, Taylor Arthur, Barnwell Richard W, and 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.
Знайти повний текст джерелаHu, 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.
Знайти повний текст джерелаChi-Wang, Shi, and 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.
Знайти повний текст джерелаChi-Wang, Shi, and 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.
Знайти повний текст джерелаA, Felippa Carlos, Park K. C, and 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.
Знайти повний текст джерелаA, Felippa Carlos, Park K. C, and 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.
Знайти повний текст джерелаB, Ransom Jonathan, Aminpour Mohammad A, and 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.
Знайти повний текст джерелаB, Ransom J., Aminpour M. A, and 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.
Знайти повний текст джерелаB, Ransom Jonathan, Aminpour Mohammad A, and 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.
Знайти повний текст джерелаGeorge, 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.
Знайти повний текст джерелаGeorge, 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.
Знайти повний текст джерелаZhang, Yong-Tao. High order WENO schemes for Hamilton-Jacobi equations on triangular meshes. Hampton, Va: ICASE, NASA Langley Research Center, 2001.
Знайти повний текст джерелаC, Hall Kenneth, and 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.
Знайти повний текст джерелаS, Liou M., and 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.
Знайти повний текст джерелаMeng-Sing, Liou, and 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.
Знайти повний текст джерелаLewis 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.
Знайти повний текст джерелаCenter, Langley Research, ed. A novel shape parameterization approach. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаCenter, Langley Research, and 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.
Знайти повний текст джерелаRupak, Biswas, Gabow Harold N, and 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.
Знайти повний текст джерелаLiseĭkin, V. D. Grid generation methods. Berlin: Springer, 1999.
Знайти повний текст джерелаCarey, Graham F. Computational grids: Generation, adaptation, and solution strategies. Washington, D.C: Taylor & Francis, 1997.
Знайти повний текст джерелаCenter, Langley Research, ed. Adaptive mesh stategies for the spectral element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Знайти повний текст джерелаM, Price John. Adaptive computational methods for aerothermal heating analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Знайти повний текст джерелаN, Tiwari S., and 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.
Знайти повний текст джерелаHesthaven, J. S. High-order/spectral methods on unstructured grids. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2001.
Знайти повний текст джерелаI, Warburton, and 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.
Знайти повний текст джерелаI, Warburton, and 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.
Знайти повний текст джерелаCenter, Langley Research, ed. Unstructured viscous grid generation by advancing-front method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Знайти повний текст джерелаBaden, Scott B. Structured Adaptive Mesh Refinement (SAMR) Grid Methods. New York, NY: Springer New York, 2000.
Знайти повний текст джерелаBaysal, Oktay. An overlapped grid method for multigrid, finite volume/difference flow solvers - MaGGiE. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаNguyen, Hung Lee. On the applications of algebraic grid generation methods based on transfinite interpolation. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Знайти повний текст джерелаJameson, 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.
Знайти повний текст джерелаMulti-grid methods and applications. Berlin: Springer-Verlag, 1985.
Знайти повний текст джерелаZ, Pirzadeh Shahyar, and 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.
Знайти повний текст джерелаZ, Pirzadeh Shahyar, and 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.
Знайти повний текст джерелаZ, Pirzadeh Shahyar, and 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.
Знайти повний текст джерелаZ, Pirzadeh Shahyar, and 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.
Знайти повний текст джерелаFrink, 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.
Знайти повний текст джерелаSigal, Ian Alejandro. Accuracy issues on unstructured grids. Ottawa: National Library of Canada, 2002.
Знайти повний текст джерелаSigal, Ian Alejandro. Accuracy issues on unstructured grids. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2002.
Знайти повний текст джерелаStanly, Steinberg, ed. Conservative finite-difference methods on general grids. Boca Raton: CRC Press, 1996.
Знайти повний текст джерелаWorld Conference on Boundary Elements and Other Mesh Reduction Methods (31st 2009 Wessex Institute of Technology). Mesh reduction methods: BEM/MRM XXXI. Edited by Brebbia C. A. Southampton, UK: WIT, 2009.
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