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Books on the topic 'K-omega turbulence model'

Author: Grafiati
Published: 4 June 2021
Last updated: 15 February 2022

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1

Rigby, David L. Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

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2

United States. National Aeronautics and Space Administration., ed. A k-[omega] turbulence model for quasi-three-dimensional turbomacinery flows. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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3

United States. National Aeronautics and Space Administration., ed. A k-[omega] turbulence model for quasi-three-dimensional turbomacinery flows. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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4

United States. National Aeronautics and Space Administration., ed. A k-[omega] turbulence model for quasi-three-dimensional turbomacinery flows. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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5

United States. National Aeronautics and Space Administration., ed. A k-[omega] turbulence model for quasi-three-dimensional turbomacinery flows. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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6

1925-, Georgiadis Nicholas, Orkwis Paul D, and United States. National Aeronautics and Space Administration., eds. Implementation of a two-equation K-[omega] turbulence model in NPARC. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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7

1925-, Georgiadis Nicholas, Orkwis Paul D, and United States. National Aeronautics and Space Administration., eds. Implementation of a two-equation K-[omega] turbulence model in NPARC. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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8

1925-, Georgiadis Nicholas, Orkwis Paul D, and United States. National Aeronautics and Space Administration., eds. Implementation of a two-equation K-[omega] turbulence model in NPARC. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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9

Implementation of a two-equation K-[omega] turbulence model in NPARC. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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10

Implementation of a two-equation K-[omega] turbulence model in NPARC. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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11

United States. National Aeronautics and Space Administration., ed. Application of the [kappa]-[omega] turbulence model to quasi-three-dimensional turbomachinery flows. Reston, VA: American Institute of Aeronautics and Astronautics, 1996.

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12

United States. National Aeronautics and Space Administration., ed. Application of the [kappa]-[omega] turbulence model to quasi-three-dimensional turbomachinery flows. Reston, VA: American Institute of Aeronautics and Astronautics, 1996.

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13

United States. National Aeronautics and Space Administration., ed. Application of the [kappa]-[omega] turbulence model to quasi-three-dimensional turbomachinery flows. Reston, VA: American Institute of Aeronautics and Astronautics, 1996.

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14

United States. National Aeronautics and Space Administration., ed. Application of the [kappa]-[omega] turbulence model to quasi-three-dimensional turbomachinery flows. Reston, VA: American Institute of Aeronautics and Astronautics, 1996.

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15

A, Ameri Ali, and NASA Glenn Research Center, eds. Two-equation turbulence models for prediction of heat transfer on a transonic turbine blade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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16

A, Ameri Ali, and NASA Glenn Research Center, eds. Two-equation turbulence models for prediction of heat transfer on a transonic turbine blade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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17

A, Ameri Ali, and NASA Glenn Research Center, eds. Two-equation turbulence models for prediction of heat transfer on a transonic turbine blade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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18

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.

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19

Center, NASA Glenn Research, ed. Heat transfer on a film-cooled rotating blade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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20

Heat transfer on a film-cooled rotating blade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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21

Heat transfer on a film-cooled rotating blade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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22

Center, Ames Research, ed. Improved two-equation k - [omega] turbulence models for aerodynamic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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23

Improved two-equation k - [omega] turbulence models for aerodynamic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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24

Improved two-equation k - [omega] turbulence models for aerodynamic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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25

Center, Ames Research, ed. Improved two-equation k - [omega] turbulence models for aerodynamic flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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