Książki na temat „High-Order finite element methods”

S̆olin, Pavel. Higher-order finite element methods. Boca Raton, Fla: Chapman & Hall/CRC, 2004.

Vandandoo, Ulziibayar, Tugal Zhanlav, Ochbadrakh Chuluunbaatar, Alexander Gusev, Sergue Vinitsky i Galmandakh Chuluunbaatar. High-Order Finite Difference and Finite Element Methods for Solving Some Partial Differential Equations. Cham: Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-44784-6.

University of Wales. Institute for Numerical Methods in Engineering. i Langley Research Center. Aerothermal Loads Branch., red. Finite element methods of analysis for high speed viscous flows. Hampton, Va: Aerothermal Loads Branch, Loads and Aeroelasticity Division, NASA Langley Research Center, 1987.

George C. Marshall Space Flight Center., red. Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows. Marshall Space Flight Center, Ala: NASA-Marshall Space Flight Center, 1988.

George C. Marshall Space Flight Center., red. Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows. Marshall Space Flight Center, Ala: NASA-Marshall Space Flight Center, 1988.

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

Yan, Jue. Local discontinuous Galerkin methods for partial differential equations with higher order derivates. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2002.

Hsing-jen, Chang, i Langley Research Center, red. H-P adaptive methods for finite element analysis of aerothermal loads in high-speed flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Xingren, Zhang, i Langley Research Center, red. H-P adaptive methods for finite element analysis of aerothermal loads in high-speed flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Hsing-jen, Chang, i Langley Research Center, red. H-P adaptive methods for finite element analysis of aerothermal loads in high-speed flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

United States. National Aeronautics and Space Administration., red. 3-D inelastic analysis methods for hot section components.: Third annual status report. [Washington, DC]: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration., red. 3-D inelastic analysis methods for hot section components.: Fourth annual status report for the period February 14, 1986 to February 14, 1987. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Center, Langley Research, red. Preliminary structural sizing of a Mach 3.0 high-speed civil transport model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Sehmi, N. S. Large order structural eigenanalysis techniques: Algorithms for finite element systems. Chichester, West Sussex, England: Ellis Horwood, 1989.

H, Carpenter Mark, i Institute for Computer Applications in Science and Engineering., red. High order finite difference methods, multidimensional linear problems and curvilinear coordinates. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1999.

Gustafsson, Bertil. High-order centered difference methods with sharp shock resolution. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1994.

Bertil, Gustafsson. High-order centered difference methods with sharp shock resolution. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1994.

Robert, Lucas, Raefsky Arthur i United States. National Aeronautics and Space Administration., red. Using a multifrontal sparse solver in a high performance finite element code. [Washington, DC: National Aeronautics and Space Administration, 1990.

Center, Langley Research, red. High order finite difference and finite volume WENO schemes and discontinuous Galerkin methods for CFD. Hampton, Va: ICASE, NASA Langley Research Center, 2001.

High order difference methods for time dependent PDE. Berlin: Springer, 2008.

Reddy, J. N. A higher-order theory for geometrically nonlinear analysis of composite laminates. Hampton, Va: Langley Research Center, 1987.

Fox, Ulrich. Finite-Elemente-Simulation von Hochtemperatur-Düsenströmungen. Aachen: Shaker, 1999.

Qu, Zu-Qing. Model Order Reduction Techniques: With Applications in Finite Element Analysis. London: Springer London, 2004.

United States. National Aeronautics and Space Administration., red. A finite element computational method for high Reynolds number laminar flows. [Washington, DC: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration., red. A velocity-pressure integrated, mixed interpolation, Galerkin finite element method for high Reynolds number laminar flows: Final report. [Washington, DC?]: Universities Space Research Association, Systems Dynamics Laboratory, Science and Engineering Directorate, 1988.

United States. National Aeronautics and Space Administration., red. A velocity-pressure integrated, mixed interpolation, Galerkin finite element method for high Reynolds number laminar flows: Final report. [Washington, DC?]: Universities Space Research Association, Systems Dynamics Laboratory, Science and Engineering Directorate, 1988.

Shigemi, Masashi. Finite element analysis of incompressible viscous flows around single and multi-element aerofoils in high Reynolds number region. Tokyo: National Aerospace Laboratory, 1988.

F, Knight Norman, Davis D. Dale, United States. Army Aviation Research and Technology Activity. i Langley Research Center, red. High-performance equation solvers and their impact on finite element analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Zingg, D. W. A review of high-order and optimized finite-difference methods for simulating linear wave phenomena. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1996.

Zingg, D. W. A review of high-order and optimized finite-difference methods for simulating linear wave phenomena. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1996.

Zingg, D. W. A review of high-order and optimized finite-difference methods for simulating linear wave phenomena. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1996.

Mulder, T. F. O. De. FEGAS: A finite element solver for 2D viscous incompressible gas flows using SUPG/PSPG stabilized piecewise linear equal-order velocity-pressure interpolation on unstructured triangular grids. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1994.

H, Carpenter Mark, i Institute for Computer Applications in Science and Engineering., red. Boundary and interface conditions for high order finite difference methods applied to the Euler and Navier-Stokes equations. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

United States. National Aeronautics and Space Administration., red. SEADYN analysis of a tow line for a high altitude towed glider: Under contract NAS3-27186. [Washington, DC: National Aeronautics and Space Administration, 1996.

T. F. O. de Mulder. FEGAS: A finite element solver for 2D viscous incompressible gas flows using SUPG/PSPG stabilized piecewise linear equal-order velocity-pressure interpolation on unstructured triangular grids. Rhode-Saint-Genèse, Belgium: Von Karman Institute for Fluid Dynamics, 1994.

United States. National Aeronautics and Space Administration., red. Multi-dimensional high order essentially non-oscillatory finite difference methods in generalized coordinates: Semi-annual progress report of NASA Langley, grant, NAG1-1145. [Washington, DC: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., red. Multi-dimensional high order essentially non-oscillatory finite difference methods in generalized coordinates: Semi-annual progress report of NASA Langley, grant, NAG1-1145. [Washington, DC: National Aeronautics and Space Administration, 1992.

C, Chamis C., i United States. National Aeronautics and Space Administration., red. Microfracture in high temperature metal matrix crossply laminates. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Rimkus, Wolfgang. Simulation and optimisation of the Interior High Pressure (IHP) manufacturing process using the Finite Element Method (FEA). Wolverhampton: University of Wolverhampton, 2000.

Shima, Eiji. Numerical analysis of multiple element high lift devices by Navier Stokes equation using implicit TVD finite volume method. New York: AIAA, 1988.

Abdul-Aziz, Ali. Structural evaluation of a space main engine (SSME) high pressure fuel turbopump turbine blade. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.

Abdul-Aziz, Ali. Structural evaluation of a space main engine (SSME) high pressure fuel turbopump turbine blade. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.

Pester, Cornelia. A posteriori error estimation for non-linear eigenvalue problems for differential operators of second order with focus on 3D vertex singularities. Berlin: Logos-Verl., 2006.

G, Horta Lucas, i Langley Research Center, red. Taxiing, take-off, and landing simulation of the high speed civil transport aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

G, Horta Lucas, i Langley Research Center, red. Taxiing, take-off, and landing simulation of the high speed civil transport aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

G, Horta Lucas, i Langley Research Center, red. Taxiing, take-off, and landing simulation of the high speed civil transport aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

G, Horta Lucas, i Langley Research Center, red. Taxiing, take-off, and landing simulation of the high speed civil transport aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

E, Wilt Thomas, i United States. National Aeronautics and Space Administration., red. Final technical report for the development of computational techniques for the nonlinear analysis of composite structures at high temperature: NASA grant number, NCC3-248, grant duration, January 13, 1992 to March 1, 1995. Toledo, Ohio: Dept. of Mechnical, Industrial and Manufacturing Engineering, University of Toledo, 1996.

L, Spanyer K., i George C. Marshall Space Flight Center., red. A study on strength evaluations of EDNi/EDCu/NARloy-Z bonded joints. [Huntsville, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

Conference on Multi-scale and High-contrast PDE: from Modelling, to Mathematical Analysis, to Inversion (2011 Oxford, England). Multi-scale and high-contrast PDE: From modelling, to mathematical analysis, to inversion : Conference on Multi-scale and High-contrast PDE:from Modelling, to Mathematical Analysis, to Inversion, June 28-July 1, 2011, University of Oxford, United Kingdom. Redaktorzy Ammari Habib, Capdeboscq Yves 1971- i Kang Hyeonbae. Providence, R.I: American Mathematical Society, 2010.