Books on the topic 'Two-dimensional viscous flow'

Turkel, Eli. Multigrid for hypersonic viscous two- and three-dimensional flows. Institute for Computer Applications in Science and Engineering, 1991.

Kim, Y. N. Computation of multi-dimensional viscous supersonic jet flow. Lewis Research Center, 1986.

Greywall, Mahesh S. Computation of three-dimensional flows using two stream functions. Wichita State University, National Institute for Aviation Research, 1991.

Lafe, O. A global interpolation function (GIF) boundary element code for viscous flows. American Institute of Aeronautics and Astronautics, 1995.

Steinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Steinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. Lewis Research Center, 1989.

Harloff, G. J. Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off design conditions. National Aeronautics and Space Administration, 1988.

Harloff, G. J. Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off design conditions. National Aeronautics and Space Administration, 1988.

Danowitz, Jeffrey S. A far-field non-reflecting boundary condition for two-dimensional wake flows. Institute for Computer Applications in Science and Engineering, 1995.

Ramamurti, R. Simulation of two-dimensional viscous flow through cascades using a semi-elliptic analysis and hybrid C-H grids. Lewis Research Center, 1988.

Abbas, Kassim K. An investigation of viscous two-dimensional two-phase flows in cascades of steam turbine blading by time-marching method. University of Birmingham, 1987.

Center, Ames Research, ed. Aerodynamic interaction between vortical wakes and lifting two-dimensional bodies. National Aeronautics and Space Administration, Ames Research Center, 1989.

Center, Ames Research, ed. Aerodynamic interaction between vortical wakes and lifting two-dimensional bodies. National Aeronautics and Space Administration, Ames Research Center, 1989.

Time-evolving bubbles in two-dimensional stokes flow. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

L, Vasconcelos Giovani, and Institute for Computer Applications in Science and Engineering., eds. Time-evolving bubbles in two-dimensional stokes flow. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

L, Vasconcelos Giovani, and Institute for Computer Applications in Science and Engineering., eds. Time-evolving bubbles in two-dimensional stokes flow. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

Parallelization of a multigrid incompressible viscous cavity flow solver using openMP. National Aeronautics and Space Administration, Langley Research Center, 1999.

G, Kunik William, and United States. National Aeronautics and Space Administration., eds. Two- and three-dimensional viscous computations of a hypersonic inlet flow. National Aeronautics and Space Administration, 1987.

Two- and three-dimensional viscous computations of a hypersonic inlet flow. National Aeronautics and Space Administration, 1987.

C, Buggeln R., McDonald H. 1937-, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Computation of multi-dimensional viscous supersonic jet flow. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Computation of multi-dimensional viscous supersonic jet flow. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

R, Reddy D., Cheng A. H. -D, and United States. National Aeronautics and Space Administration., eds. A global interpolation function (GIF) boundary element code for viscous flows. American Institute of Aeronautics and Astronautics, 1995.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Institute for Computer Applications in Science and Engineering. and United States. National Aeronautics and Space Administration., eds. Directional agglomeration multigrid techniques for high-Reynolds number viscous flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

Institute for Computer Applications in Science and Engineering., ed. Directional agglomeration multigrid techniques for high-Reynolds number viscous flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

Oktay, Baysal, and United States. National Aeronautics and Space Administration., eds. Wing-section optimization for supersonic viscous flow: [abstract]. National Aeronautics and Space Administration, 1995.

Oktay, Baysal, and United States. National Aeronautics and Space Administration., eds. Wing-section optimization for supersonic viscous flow: [abstract]. National Aeronautics and Space Administration, 1995.

Oktay, Baysal, and United States. National Aeronautics and Space Administration., eds. Wing-section optimization for supersonic viscous flow: [abstract]. National Aeronautics and Space Administration, 1995.

1931-, Abarbanel Saul S., Turkel E, and Institute for Computer Applications in Science and Engineering., eds. A far-field non-reflecting boundary condition for two-dimensional wake flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

A far-field non-reflecting boundary condition for two-dimensional wake flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

A far-field non-reflecting boundary condition for two-dimensional wake flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

P, Van Dam C., and United States. National Aeronautics and Space Administration., eds. Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data: Final report. Dept. of Mechanical and Aeronautical Engineering, University of California, 1995.

P, Van Dam C., and United States. National Aeronautics and Space Administration., eds. Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data: Final report. Dept. of Mechanical and Aeronautical Engineering, University of California, 1995.

P, Van Dam C., and United States. National Aeronautics and Space Administration., eds. Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data: Final report. Dept. of Mechanical and Aeronautical Engineering, University of California, 1995.

Urmila, Ghia, Ghia K. N, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Simulation of two-dimensional viscous flow through cascades using a semi-elliptic analysis and hybrid C-H grids. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Urmila, Ghia, Ghia K. N, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Simulation of two-dimensional viscous flow through cascades using a semi-elliptic analysis and hybrid C-H grids. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Center, Langley Research, ed. The variational method for aerodynamic optimization using the Navier-Stokes equations: Prepared for Langley Research Center under contract NAS1-19480. National Aeronautics and Space Administration, Langley Research Center, 1997.

E, Turkel, and Langley Research Center, eds. Multigrid for hypersonic viscous two-and three-dimensional flows. National Aeronautics and Space Administration, Langley Research Center, 1991.

M, Napolitano, and Institute for Computer Applications in Science and Engineering, eds. Efficient solutions of two-dimensional incompressible steady viscous flows. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1986.

United States. National Aeronautics and Space Administration., ed. A diagonally inverted LU implicit multigrid scheme for the 3-D Navier-Stokes equations and a two equation model of turbulence. National Aeronautics and Space Administration, 1988.