Books on the topic 'Volume of Fluid (VOF) method'

Whitaker, Stephen. The method of volume averaging. Kluwer Academic, 1999.

Moukalled, F., L. Mangani, and M. Darwish. The Finite Volume Method in Computational Fluid Dynamics. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-16874-6.

1960-, Malalasekera W., ed. An introduction to computational fluid dynamics: The finite volume method. 2nd ed. Pearson Education Ltd., 2007.

Jr, N. C. Reis. Finite volume method to solve free surface fluid flow problems. UMIST, 1997.

1960-, Malalasekera W., ed. An introduction to computational fluid dynamics: The finite volume method. New York, 1995.

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

Center, Lewis Research, ed. A control-volume method for analysis of unsteady thrust augmenting ejector flows. Lewis Research Center, National Aeronautics and Space Administration, 1988.

Center, Lewis Research, ed. A control-volume method for analysis of unsteady thrust augmenting ejector flows. Lewis Research Center, National Aeronautics and Space Administration, 1988.

Wood, William A. Comments on the diffusive behavior of two upwind schemes. National Aeronautics and Space Administration, Langley Research Center, 1998.

Wood, William A. Comments on the diffusive behavior of two upwind schemes. National Aeronautics and Space Administration, Langley Research Center, 1998.

L, Whitfield David, Anderson W. Kyle, and United States. National Aeronautics and Space Administration., eds. An multiblock approach for calculating incompressible fluid flows on unstructured grids. National Aeronautics and Space Administration, 1997.

Klinger, L. Simulation numérique 3D d'une torche à plasma par une méthode de volumes finis. Centre de Recherches en Physique des Plasmas, Ecole Polytechnique Fédérale de Lausanne, 2002.

American Society of Mechanical Engineers. Winter Meeting. Numerical methods for compressible flows: Finite difference, element, and volume techniques : presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Anaheim, California, December 7-12, 1986. ASME, 1986.

Dimitri, Mavriplis, and Institute for Computer Applications in Science and Engineering., eds. Implicit method for the computation of unsteady flows on unstructured grids. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

Dimitri, Mavriplis, and Institute for Computer Applications in Science and Engineering., eds. Implicit method for the computation of unsteady flows on unstructured grids. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

Singh, Jatinder. An adaptive flow solver for air-borne vehicles undergoing time-dependent motions/deformations: Annual technical progress report, period--August 1, 1996 - July 31, 1997, NASA grant no.--NAG-1-1760. National Aeronautics and Space Administration, 1997.

Massey, Steven James. Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff. National Aeronautics and Space Administration, Langley Research Center, 2001.

Center, NASA Glenn Research, ed. Euler flow computations on non-matching unstructured meshes. National Aeronautics and Space Administration, Glenn Research Center, 1999.

A, Waithe Kenrick, and Langley Research Center, eds. Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff. National Aeronautics and Space Administration, Langley Research Center, 2001.

Center, NASA Glenn Research, ed. Euler flow computations on non-matching unstructured meshes. National Aeronautics and Space Administration, Glenn Research Center, 1999.

Felici, Helene M. A coupled Eulerian/Lagrangian method for the solution of three-dimensional vortical flows. Gas Turbine Laboratory, Massachusetts Institute of Technology, 1992.

Felici, Helene M. A coupled Eulerian/Lagrangian method for the solution of three-dimensional vortical flows. National Aeronautics and Space Administration, 1992.

Tuncer, Cebeci, ed. Computational fluid dynamics for engineers: From panel to Navier-Stokes methods with computer programs. Horizons Pub. Inc., 2005.

United States. National Aeronautics and Space Administration., ed. An experimental and numerical investigation of turbulent vortex breakdown and aircraft wakes: Final report, contract NAG 1-1775. National Aeronautics and Space Administration, 1996.

Ethiraj, Venkatapathy, and Ames Research Center, eds. SAGE, the self-adaptive grid codE, version 3. National Aeronautics and Space Administration, Ames Research Center, 1999.

Ethiraj, Venkatapathy, and Ames Research Center, eds. SAGE, the self-adaptive grid codE, version 3. National Aeronautics and Space Administration, Ames Research Center, 1999.

Ethiraj, Venkatapathy, and Ames Research Center, eds. SAGE, the self-adaptive grid codE, version 3. National Aeronautics and Space Administration, Ames Research Center, 1999.

Ethiraj, Venkatapathy, and Ames Research Center, eds. SAGE, the self-adaptive grid codE, version 3. National Aeronautics and Space Administration, Ames Research Center, 1999.

G, Chen, and United States. National Aeronautics and Space Administration., eds. A computational fluid dynamic and heat transfer model for gaseous core and gas cooled space power and propulsion reactors. National Aeronautics and Space Administration, 1996.

Institute for Computer Applications in Science and Engineering., ed. Implicit schemes and parallel computing in unstructured grid CFD. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

Institute for Computer Applications in Science and Engineering., ed. Implicit schemes and parallel computing in unstructured grid CFD. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

United States. National Aeronautics and Space Administration., ed. Development of an upwind, finite-volume code with finite-rate chemistry. MCAT Institute, 1994.

United States. National Aeronautics and Space Administration., ed. Development of an upwind, finite-volume code with finite-rate chemistry. MCAT Institute, 1995.

Coirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. American Institute of Aeronautics and Astronautics, 1996.

A, Ameri Ali, Rigby David L, and United States. National Aeronautics and Space Administration., eds. Simulations of turbine cooling flows using a multiblock-multigrid scheme: Under cooperative agreement NCC3-370. National Aeronautics and Space Administration, 1996.

M, Sindir Munir, and United States. National Aeronautics and Space Administration., eds. Comparative study of advanced turbulence models for turbomachinery: Contract NAS8-38860, final report. National Aeronautics and Space Administration, 1996.

A, Ameri Ali, Rigby David L, and United States. National Aeronautics and Space Administration., eds. Simulations of turbine cooling flows using a multiblock-multigrid scheme: Under cooperative agreement NCC3-370. National Aeronautics and Space Administration, 1996.

Coirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. American Institute of Aeronautics and Astronautics, 1996.

N, Tiwari S., and United States. National Aeronautics and Space Administration., eds. Drag reduction on circular cylinders by ejecting jet from rear stagnation region: Progress report for the period ending June 30, 1997 ... under Cooperative Agreement NCC1-232. Dept. of Mechanical Engineering, College of Engineering and Technology, Old Dominion University, 1997.

A, Ameri Ali, Rigby David L, and United States. National Aeronautics and Space Administration., eds. Simulations of turbine cooling flows using a multiblock-multigrid scheme: Under cooperative agreement NCC3-370. National Aeronautics and Space Administration, 1996.

Coirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. American Institute of Aeronautics and Astronautics, 1996.

Coirier, William J. Solution-adaptive Cartesian cell approach for viscous and inviscid flows. American Institute of Aeronautics and Astronautics, 1996.

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

Center, 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. National Aeronautics and Space Administration, Langley Research Center, 1998.

Z, Pirzadeh Shahyar, and Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. National Aeronautics and Space Administration, Langley Research Center, 1998.

Frink, Neal T. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. National Aeronautics and Space Administration, Langley Research Center, 1998.

Z, Pirzadeh Shahyar, and Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. National Aeronautics and Space Administration, Langley Research Center, 1998.

Z, Pirzadeh Shahyar, and Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. National Aeronautics and Space Administration, Langley Research Center, 1998.