Książki na temat „Lagrange equations”

United States. National Aeronautics and Space Administration., red. Eno-Oshers schemes for Euler equations. [Washington, DC]: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., red. Eno-Oshers schemes for Euler equations. [Washington, DC]: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., red. Eno-Osher schemes for Euler equations. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Huynh, Hung T. Accurate upwind methods for the Euler equations. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Fuhrer, Claus. Formulation and numerical solution of the equations of constrained mechanical motion. Koln: DFLVR, 1989.

Ajay, Kumar, i Langley Research Center, red. Compact high order schemes for the Euler equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Center, Langley Research, red. Singularities of the Euler equation and hydrodynamic stability. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

E, Turkel, i United States. National Aeronautics and Space Administration., red. Central difference TVD and TVB schemes for time dependent and steady state problems. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Center, Langley Research, red. Singularities of the Euler equation and hydrodynamic stability. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

M, Atassi H., i United States. National Aeronautics and Space Administration., red. Numerical solutions of the linearized Euler equations for unsteady vortical flows around lifting airfoils. [Washington, DC: National Aeronautics and Space Administration, 1990.

R, Chakravarthy Sukumar, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. A user guide for the EMTAC-MZ CFD code. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Walters, Robert W. Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions. [Washington, DC]: National Aeronautics and Space Administration Scientific and Technical Information Branch, 1987.

Walters, Robert W. Efficient solutions to the Euler equations for supersonic flow with embedded subsonic regions. [Washington, DC]: National Aeronautics and Space Administration Scientific and Technical Information Branch, 1987.

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

Chen, Robert T. N. Flap-lag equations of motion of rigid, articulated rotor blades with three hinge sequences. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Center, Ames Research, red. Patched-grid calculations with the Euler and Navier-Stokes equations: Theory and application. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

E, Turkel, Schaffer Steve i United States. National Aeronautics and Space Administration., red. Comparison of three explicit multigrimethods for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1987.

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

Air Resources Laboratory (U.S.), red. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

Center, Ames Research, red. Flap-lag equations of motion of rigid, articulated rotor blades with three hinge sequences. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Center, Ames Research, red. Patched-grid calculations with the Euler and Navier-Stokes equations: Theory and application. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

Center, Langley Research, red. A numerical resolution study of high order essentially non-oscillatory schemes applied to recompressible flow. Hampton, Va: ICASE, National Aeronautics and Space Administration, Langley Research Center, 1992.

Center, Ames Research, red. Flap-lag equations of motion of rigid, articulated rotor blades with three hinge sequences. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Center, Ames Research, red. Patched-grid calculations with the Euler and Navier-Stokes equations: Theory and application. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

Chen, Robert T. N. Flap-lag equations of motion of rigid, articulated rotor blades with three hinge sequences. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

Draxler, Roland R. Hybrid single-particle Lagrangian integrated trajectories (HY-SPLIT): Model description. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, 1988.

Milev, Ivo. Integrierte Modelle zur physikalischen Interpretation geodatischer Deformationsuntersuchungen. Munchen: Verlag der Bayerischen Akademie der WissenschaftKommission bei der C.H. Beck'schen Verlagsbuchhandlung, 2001.

Center, Ames Research, red. Solution of nonlinear flow equations for complex aerodynamic shapes. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1992.

Center, Ames Research, red. Solution of nonlinear flow equations for complex aerodynamic shapes. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1992.

Bennett, Andrew F. Lagrangian fluid dynamics. Cambridge: Cambridge University Press, 2005.

Sporykhin, A. N. Kombinirovannyĭ podkhod Ėĭlera-Lagranzha v mekhanike sploshnoĭ sredy. Voronezh: Izd-vo Voronezhskogo universiteta, 1991.

Kumar, Jain Romesh, red. Solution of two-dimensional Euler equations: Experience with a finite volume code. Köln: DFVLR, 1987.

Center, Langley Research, red. Canonical forms of multidimensional steady inviscid flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

United States. National Aeronautics and Space Administration., red. Structural optimization of large structural systems by optimality criteria methods. [Washington, DC: National Aeronautics and Space Administration, 1992.

X, Ying S., Ames Research Center i United States. Army Aviation Systems Command. Army Aviation Research and Technology Activity., red. Euler solution of multiblade rotor flow. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Meĭrmanov, A. M. Evolution equations and Lagrangian coordinates. Berlin: Walter de Gruyter, 1997.

Dehn, Edgar. Algebraic equations: An introduction to the theories of Lagrange and Galois. Mineola, N.Y: Dover Publications, 2004.

Center, Langley Research, red. Three dimensional unstructured multigrid for the Euler equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

J, Mavriplis D., i Langley Research Center, red. Agglomeration multigrid for the three-dimensional Euler equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Anderson, W. Kyle. Accurate solutions, parameter studies, and comparisons for the Euler and potential flow equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

McDonald, Aidan. The origin of noise in semi-Lagrangian integrations. Dublin: Met Éireann, 1998.

Posiadała, Bogdan. Modelowanie i analiza drgań ciągło-dyskretnych układów mechanicznych: Zastosowanie formalizmu mnożników Lagrange'a. Częstochowa: Wydawn. Politechniki Częstochowskiej, 2007.

Jentink, Thomas Neil. Formulation of boundary conditions for the multigrid acceleration of the Euler and Navier Stokes equations. West Lafayette, Ind: Purdue University, School of Aeronautics and Astronautics, 1990.

INRIA Workshop on Numerical Methods for the Euler Equations of Fluid Dynamics (1983 Rocquencourt, Yvelines, France). Numerical methods for the Euler equations of fluid dynamics. Philadelphia: Society for Industrial and Applied Mathematics, 1985.

Șandru, Ovidiu-Ilie. Local Hamilton-Lagrange structures: Applications in the partial differential equations theory. Timișoara: Universitatea din Timișoara, Facultatea de Matematică, 1994.

Rossow, Cord-Christian. Berechnung von Strömungsfeldern durch Lösung der Euler-Gleichungen mit einer erweiterten Finite-Volumen Diskretisierungsmethode. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1989.

L, Van Dommelen Leon, Lam Shui T i Langley Research Center, red. On the use of Lagrangian variables in descriptions of unsteady boundary-layer separation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Giachetta, G. Advanced classical field theory. Hackensack, NJ: World Scientific, 2009.