Livres sur le sujet « 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 et 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. et Langley Research Center. Aerothermal Loads Branch., dir. 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., dir. 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., dir. 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, et Langley Research Center, dir. 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, et Langley Research Center, dir. 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, et Langley Research Center, dir. 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., dir. 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., dir. 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, dir. 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, et Institute for Computer Applications in Science and Engineering., dir. 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 et United States. National Aeronautics and Space Administration., dir. Using a multifrontal sparse solver in a high performance finite element code. [Washington, DC : National Aeronautics and Space Administration, 1990.

Center, Langley Research, dir. 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., dir. 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., dir. 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., dir. 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. et Langley Research Center, dir. 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, et Institute for Computer Applications in Science and Engineering., dir. 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., dir. 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., dir. 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., dir. 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., et United States. National Aeronautics and Space Administration., dir. 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, et Langley Research Center, dir. 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, et Langley Research Center, dir. 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, et Langley Research Center, dir. 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, et Langley Research Center, dir. 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, et United States. National Aeronautics and Space Administration., dir. 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., et George C. Marshall Space Flight Center., dir. 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. Sous la direction de Ammari Habib, Capdeboscq Yves 1971- et Kang Hyeonbae. Providence, R.I : American Mathematical Society, 2010.