Books on the topic 'K-epsilon turbulence model'

Mohammadi, B. Analysis of the K-epsilon turbulence model. Chichester: Wiley, 1993.

Nikjooy, Mohammad. K-epsilon turbulence model assessment with reduced numerical diffusion for coaxial jets. New York: AIAA, 1988.

Speziale, Charles G. Numerical solution of turbulent flow past a backward facing step using a nonlinear K-epsilon model. Hampton, Va: ICASE, 1987.

Chu, Chiang. Calculations of diffuser flows with an anisotropic K-[epsilon] model. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Zhu, Jiang. Calculations of diffuser flows with an anisotropic K-[epsilon] model. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Bernard, Peter S. Bounded energy states in homogeneous turbulent shear flow, an alternative view. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1990.

Lee, J. An application of a two-equation model of turbulence to three-dimensional chemically reacting flows. [Washington, DC: National Aeronautics and Space Administration, 1994.

Lee, J. An application of a two-equation model of turbulence to three-dimensional chemically reacting flows. [Washington, DC: National Aeronautics and Space Administration, 1994.

Abdol-Hamid, Khaled S. Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Abdol-Hamid, Khaled S. Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Abdol-Hamid, Khaled S. Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Aichouni, Mohamed. Development and decay of turbulent pipe flows: An experimental and computational study. Salford: Universityof Salford, 1992.

Bauer, Christopher. Low Reynolds number [kappa]-[epsilon] and empirical transition models for oscillatory pipe flow and heat transfer. [Washington, D.C: National Aeronautics and Space Administration, 1993.

Kwon, Okey. Advanced k-epsilon modeling of heat transfer. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

Kwon, Okey. Advanced k-epsilon modeling of heat transfer. Cleveland, Ohio: Lewis Research Center, 1995.

Khalid, M. Turbulent boundary layer solution for two-dimensional compressible flow using mixing length and K-[epsilon] turbulence models. Ottawa: National Research Council Canada, 1990.

Liu, Jong-Shang. Navier-Stokes cascade analysis with a stiff K-epsilon turbulence solver. Cleveland: Institute for Computational Mechanics in Propulsion, Lewis Research Center, 1987.

Błazik-Borowa, Ewa. Problemy związane ze stosowaniem modelu turbulencji k-[epsilon] do wyznaczania parametrów opływu budynków. Lublin: Wydawnictwo Politechniki Lubelskiej, 2008.

Sang-Wook, Kim, and United States. National Aeronautics and Space Administration., eds. Computation of turbulent flows using an extended k-[epsilon] turbulence closure model. [Washington, DC: National Aeronautics and Space Administration, 1987.

W, Kim S., and United States. National Aeronautics and Space Administration, eds. Computation of turbulent flows using an extended k-[epsilon] turbulence closure model. [Washington, DC: National Aeronautics and Space Administration, 1987.

H, Shih T., and United States. National Aeronautics and Space Administration., eds. A Galilean and tensorial invariant k-[epsilon] model for near wall turbulence. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Modification of the two-equation turbulence model in NPARC to a Chien low Reynolds number k-epsilon formulation. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Tawit, Chitsomboon, Zu Jiang, and United States. National Aeronautics and Space Administration., eds. Modification of the two-equation turbulence model in NPARC to a Chien low Reynolds number k-epsilon formulation. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Modification of the two-equation turbulence model in NPARC to a Chien low Reynolds number k-epsilon formulation. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Tuan, Ngo, and Institute for Computer Applications in Science and Engineering., eds. Numerical solution of turbulent flow past a backward facing step using a nonlinear K-[epsilon] model. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1987.

An improved [k-epsilon] model for near-wall turbulence and comparison with direct numerical simulation. [Washington, DC: National Aeronautics and Space Administration, 1990.

H, Pletcher Richard, Van Dalsem William R, and United States. National Aeronautics and Space Administration., eds. Wall functions for the k- [epsilon] turbulence model in generalized nonorthogonal curvilinear coordinates: Final report. [Ames, Iowa?]: Heat Transfer Laboratory, Dept. of Mechanical Engineering, Computational Fluid Dynamics Center, Engineering Research Institute, Iowa State University, 1992.

An improved [k-epsilon] model for near-wall turbulence and comparison with direct numerical simulation. [Washington, DC: National Aeronautics and Space Administration, 1990.

United States. National Aeronautics and Space Administration., ed. An improved [k-epsilon] model for near-wall turbulence and comparison with direct numerical simulation. [Washington, DC: National Aeronautics and Space Administration, 1990.

J, Georgiadis Nicholas, NASA Glenn Research Center, and United States. National Aeronautics and Space Administration., eds. Implementation and validation of the Chien k-[epsilon] turbulence model in the Wind Navier-Stokes code. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Ridha, Abid, and United States. National Aeronautics and Space Administration., eds. Prediction of complex aerodynamic flows with explicit algebraic stress models: 34th Aerospace Sciences Meeting & Exhibit, January 15-18, 1996/Reno, NV. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

B, Gatski T., and NASA Glenn Research Center, eds. Summary of EASM turbulence models in CFL3D with validation test cases. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.

H, Shih T., and United States. National Aeronautics and Space Administration., eds. A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers. [Washington, D.C.]: NASA, 1992.

H, Shih T., and United States. National Aeronautics and Space Administration., eds. A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers. [Washington, D.C.]: NASA, 1992.

H, Shih T., and United States. National Aeronautics and Space Administration., eds. A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers. [Washington, D.C.]: NASA, 1992.

A critical evaluation of two-equation models for near wall turbulence. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1990.

Turbulence modeling validation, testing, and development. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.

Computation of supersonic jet mixing noise for an axisymmetric CD nozzle using k-(epsilon) turbulence model. [Washington, DC: National Aeronautics and Space Administration, 1991.

1940-, Shih Tsan-Hsing, and Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. A k-[epsilson] modeling of near wall turbulence. Cleveland, Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1991.

1940-, Shih Tsan-Hsing, and Lewis Research Center. Institute for Computational Mechanics in Propulsion, eds. A k-[epsilson] modeling of near wall turbulence. Cleveland, Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1991.

A k-[epsilson] modeling of near wall turbulence. Cleveland, Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1991.

1940-, Shih Tsan-Hsing, and Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. A k-[epsilson] modeling of near wall turbulence. Cleveland, Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1991.

United States. National Aeronautics and Space Administration., ed. An application of a two-equation model of turbulence to three-dimensional chemically reacting flows. [Washington, DC: National Aeronautics and Space Administration, 1994.

C, Hendricks Robert, Steinetz Bruce M, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of flow in a whirling annular seal and comparison with experiments. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Lewis Research Center. Institute for Computational Mechanics in Propulsion., ed. Effects of artificial viscosity on the accuracy of high-Reynolds-number [kappa-epsilon] turbulence model. Cleveland, Ohio: NASA, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1994.

Tawit, Chitsomboon, Zu Jiang, and United States. National Aeronautics and Space Administration., eds. Modification of the two-equation turbulence model in NPARC to a Chien low Reynolds number k-epsilon formulation. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Lewis Research Center. Institute for Computational Mechanics in Propulsion., ed. Calculation of 3D turbulent jets in crossflow with a multigrid method and a second-moment closure model. Cleveland,Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1990.

-H, Shih T., and United States. National Aeronautics and Space Administration., eds. An NPARC turbulence module with wall functions: Under cooperative agreement NCC3-370. [Washington, DC]: National Aeronautics and Space Administration, 1997.

1940-, Shih Tsan-Hsing, and United States. National Aeronautics and Space Administration., eds. Low Reynolds number two-equation modeling of turbulent flows. [Washington, D.C.]: NASA, 1991.

Low Reynolds number two-equation modeling of turbulent flows. [Washington, D.C.]: NASA, 1991.