Books on the topic 'Euler Equation'

Lettau, Martin. Euler equation errors. Cambridge, MA: National Bureau of Economic Research, 2005.

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

Landis, Markley F., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Minimal parameter solution of the orthogonal matrix differential equation. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Cannizzaro, Frank E. A multiblock multigrid three-dimensional Euler equation solver. [S.l.]: [s.n.], 1991.

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

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

Kujii, Kozo. Evaluation of Euler and Navier-Stokes solutions for leading-edge and shock-induced separations. Chofu, Tokyo, Japan: National Aerospace Laboratory, 1985.

Center, Langley Research, ed. Canonical-variables multigrid method for steady-state Euler equation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Farhi, Emmanuel. Capital taxation: Quantitative exploration of the inverse Euler equation. Cambridge, MA: Massachusetts Institute of Technology, Dept. of Economics, 2005.

Farhi, Emmanuel. Capital taxation: Quantitative explorations of the Inverse Euler equation. Cambridge, MA: Massachusetts Institute of Technology, Dept. of Economics, 2009.

Abarbanel, Saul. Splitting methods for low Mach number Euler and Navier-Stokes equations. Hampton, Va: ICASE, 1987.

Tanveer, Saleh. A Note on singularities of the 3-D Euler equation. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Mavriplis, Dimitri J. Euler and Navier-Stokes computations for two-dimensional geometries using unstructured meshes. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

1948-, Speziale C. G., and Institute for Computer Applications in Science and Engineering., eds. A modified restricted Euler equation for turbulent flows with mean velocity gradients. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Tadmor, Eitan. A minimum entropy principle in the gas dynamics equation. Hampton, Va: ICASE, 1986.

Chima, Rodrick V. Comparison of three explicit multigrid methods for the Euler and Navier-Stokes equations. Cleveland, Ohio: Lewis Research Center, 1987.

Cooper, Russell. Euler-equation estimation for discrete choice models: A capital accumulation application. Cambridge, MA: National Bureau of Economic Research, 2010.

Roberts, Thomas W. Euler equation computations for the flow over a hovering helicopter rotor. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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.

-H, Shih S., Mankbadi R. R, and United States. National Aeronautics and Space Administration., eds. Effect of coannular flow on linearized Euler equation predictions of jet noise. [Washington, DC: National Aeronautics and Space Administration, 1997.

A, Bakhle Milind, and United States. National Aeronautics and Space Administration., eds. Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver. [Washington, D.C: National Aeronautics and Space Administration, 1996.

O, Demuren A., and Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. On bi-grid local mode analysis of solution techniques for 3-D Euler and Navier-Stokes equations. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1994.

van, Leer Bram, and United States. National Aeronautics and Space Administration., eds. Numerical flux formulas for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Institute for Computer Applications in Science and Engineering., ed. Euler and Navier-Stokes computations for two-dimensional geometries using unstructured meshes. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1990.

United States. National Aeronautics and Space Administration, ed. An LU-SSOR scheme for the Euler and Navier-Stokes equations. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration, ed. An LU-SSOR scheme for the Euler and Navier-Stokes equations. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration., ed. An LU-SSOR scheme for the Euler and Navier-Stokes equations. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

Yoon, Seokkwan. An LU-SSOR scheme for the Euler and Navier-Stokes equations. New York, N. Y: American Institute of Aeronautics and Astronautics, 1987.

Lin, Kenneth Shang-Kai. Private consumption, non-traded goods and real exchange rate: A cointegration-Euler equation approach. Cambridge, MA: National Bureau of Economic Research, 1996.

Atkins, H. L. A multi-block multigrid method for the solution of the Euler and Navier-Stokes equations for three-dimensional flows. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.

E, Jorgenson Philip C., and United States. National Aeronautics and Space Administration., eds. A mixed volume grid approach for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1996.

E, Jorgenson Philip C., and United States. National Aeronautics and Space Administration., eds. A mixed volume grid approach for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1996.

H, Carpenter Mark, and Institute for Computer Applications in Science and Engineering., eds. 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.

Coirier, William J. A Cartesian, cell-based approach for adaptively-refined solutions of the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. A Cartesian, cell-based approach for adaptively-refined solutions of the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. A Cartesian, cell-based approach for adaptively-refined solutions of the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1994.

McMillin, S. Naomi. Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings: A correlation with experiment. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

McMillin, S. Naomi. Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings: A correlation with experiment. Hampton, Va: Langley Research Center, 1990.

Das, Arabindo. Numerical solution of flow fields around delta wings using Euler equation methods. Pt. II. Analysis of the results and comparison with experiments. Braunschweig: DFVLR, 1986.

E, Turkel, and Langley Research Center, eds. Multistage schemes with multigrid for Euler and Navier-Stokes equations: Components and analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

T, Batina John, Williams Marc H, and United States. National Aeronautics and Space Administration., eds. Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes. [Washington, DC]: National Aeronautics and Space Administration, 1990.

T, Batina John, Williams Marc H, and United States. National Aeronautics and Space Administration., eds. Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes. [Washington, DC]: National Aeronautics and Space Administration, 1990.

T, Batina John, Williams Marc H, and United States. National Aeronautics and Space Administration., eds. Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes. [Washington, DC]: National Aeronautics and Space Administration, 1990.

United States. National Aeronautics and Space Administration., ed. An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Coirier, William J. An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Attanasio, Orazio P. Intertemporal substitution, risk aversion and the Euler Equation for consumption: Evidence from aggregate and average cohort data. London: University College, 1987.

Amano, Robert A. The dynamic behaviour of Canadian imports and the linear-quadratic model: Evidence based on the Euler equation. [Ottawa]: Bank of Canada, 1994.

Carroll, Chris. Death to the log-linearized consumption Euler equation!: (and very poor health to the second-order approximation). Cambridge, MA: National Bureau of Economic Research, 1997.

I, Sadrehaghighi, Tiwari S. N, Langley Research Center, and Old Dominion University. Research Foundation., eds. Application of Lagrangian blending functions for grid generation around airplane geometries. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.