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1

Song, Jin-Min. Studies of confined and unconfined turbulent jet flows. Manchester: University of Manchester, 1996.

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2

Burns, A. D. Numerical prediction of turbulent three dimensional jet flows in rectangular enclosures. Oxfordshire: Computer Science and Systems Division, Harwell Laboratory, 1986.

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3

Jiang, Zhu, Lumley John L. 1930- i Lewis Research Center. Institute for Computational Mechanics in Propulsion., red. Modeling of wall-bounded complex flows and free shear flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1994.

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4

Chiang, Chu, Lumley John L. 1930- i Lewis Research Center. Institute for Computational Mechanics in Propulsion., red. Modeling of wall-bounded complex flows and free shear flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1994.

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5

Chiang, Chu, Lumley John L. 1930- i Lewis Research Center. Institute for Computational Mechanics in Propulsion., red. Modeling of wall-bounded complex flows and free shear flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1994.

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6

Villasenor, R. Modeling ideally expanded supersonic turbulent jet flows with nonpremixed H2-air combustion. Washington: American Institute of Aeronautics and Astronautics, 1990.

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7

Y, Chen J., Limley J. L i Lewis Research Center. Institute for Computational Mechanics in Propulsion., red. Second order modeling of boundary-free turbulent shear flows. Cleveland, Ohio: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1991.

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8

Ryan, Martyn J. The effect of hydrodynamic stress on plant cell cultures in turbulent jet flows. Dublin: University College Dublin, 1997.

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9

Rubinstein, Robert. Time correlations and the frequency spectrum of sound radiated by turbulent flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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10

IUTAM, Symposium (1990 Novosibirsk R. S. F. S. R. ). Separated flows and jets. Berlin: Springer-Verlag, 1991.

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11

Center, NASA Glenn Research, red. Survey of turbulence models for the computation of turbulent jet flow and noise. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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12

Center, NASA Glenn Research, red. The numerical analysis of a turbulent compressible jet. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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13

Selby, Gregory V. Jet vortex generators for turbulent flow separation control. Norfolk, Va: Old Dominion University Research Foundation, 1990.

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14

Institute for Computer Applications in Science and Engineering., red. Modeling jets in cross flow. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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15

Mankbadi, Reda R. Effects of core turbulence on jet excitability. Cleveland, Ohio: Institute for Computational Mechanics in Propulsion, 1988.

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16

Pitts, William M. Mixing in variable density, isothermal turbulent flows and implications for chemically reacting turbulent flows. Gaithersburg, MD: U.S. Dept. of Commerce, National Bureau of Standards, 1987.

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17

Pitts, William M. Mixing in variable density, isothermal turbulent flows and implications for chemically reacting turbulent flows. Gaithersburg, MD: U.S. Dept. of Commerce, National Bureau of Standards, 1987.

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18

Mankbadi, R. R. Effects of core turbulence on jet excitability. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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19

D, Cutler Andrew, i Langley Research Center, red. Effects of jet swirl on mixing of a light gas jet in a supersonic airstream. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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20

Kumar, Sanjiv. A computer model in general 3-D curvilinear coordinates for the protection of the turbulent flow field in a jet induced ram combustor. Tokyo, Japan: National Aerospace Laboratory, 1994.

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21

J, Georgiadis Nicholas, i NASA Glenn Research Center, red. An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

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22

Dembowski, Mary Ann. An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

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23

Pergament, Harold S. Hybrid two-equation turbulence model for high speed propulsive jets. New York: AIAA, 1986.

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24

Fung, K. Yin. Numerical smoothing techniques for viscous layer flows. [Downsview, Ont.]: University of Toronto, Department of Aerospace Science and Engineering, 1990.

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25

Kumar, Sanjiv. A computer model for the simulation of turbulent reacting flow in a jet assisted ram combustor. Chofu, Tokyo: National Aerospace Laboratory, 1995.

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26

Jiang, Lei-Yong. Turbulent mixing in supersonic high-temperature exhaust jets. [North York, Ont.]: University of Toronto, Institute for Aerospace Studies, 1996.

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27

Jiang, Lei-Yong. Turbulent mixing in supersonic high-temperature exhaust jets. Downsview, Ont: Institute for Aerospace Studies, University of Toronto, 1995.

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28

United States. National Aeronautics and Space Administration., red. Near-wall modelling of compressible turbulent flows. Tempe, Ariz: College of Engineering & Applied Science, Arizona State University, 1991.

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29

S, Lundgren Thomas, i United States. National Aeronautics and Space Administration., red. Effect of swirl on turbulent structures in supersonic jets: Final report, NCC2-5221. [Washington, DC: National Aeronautics and Space Administration, 1998.

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30

S, Lundgren Thomas, i United States. National Aeronautics and Space Administration., red. Effect of swirl on turbulent structures in supersonic jets: Final report, NCC2-5221. [Washington, DC: National Aeronautics and Space Administration, 1998.

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31

S, Lundgren Thomas, i United States. National Aeronautics and Space Administration., red. Large scale turbulent structures in supersonic jets. Minneapolis, MN: Dept. of Aerospace Engineering and Mechanics, University of Minnesota, 1997.

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32

S, Lundgren Thomas, i United States. National Aeronautics and Space Administration., red. Large scale turbulent structures in supersonic jets. Minneapolis, MN: Dept. of Aerospace Engineering and Mechanics, University of Minnesota, 1997.

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33

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

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34

Demuren, A. O. Characteristics of 3D turbulent jets in crossflow. [Cleveland, Ohio]: NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1991.

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35

B, Gatski T., Speziale C. G. 1948- i Institute for Computer Applications in Science and Engineering., red. On the prediction of free turbulent jets with swirl using a quadratic pressure-strain model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1994.

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36

B, Gatski T., Speziale C. G. 1948- i Institute for Computer Applications in Science and Engineering., red. On the prediction of free turbulent jets with swirl using a quadratic pressure-strain model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1994.

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37

V, Wilson Robert, i Langley Research Center, red. Streamwise vorticity generation in laminar and turbulent jets. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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38

M, Golebiowski, Seiner John M i United States. National Aeronautics and Space Administration., red. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

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39

M, Golebiowski, Seiner John M i United States. National Aeronautics and Space Administration., red. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

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40

M, Golebiowski, Seiner John M i United States. National Aeronautics and Space Administration., red. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

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41

Dash, Sanford M. Observations on practical turbulence modeling for high-speed jet/plume flowfields. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.

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42

1956-, Martin R. M., i Ames Research Center, red. Background noise measurements from jet exit vanes designed to reduce flow pulsations in an open-jet wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

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43

Abdol-Hamid, Khaled Sayed. Multiscale turbulence effects in supersonic jets exhausting into still air. Hampton, Va: Langley Research Center, 1987.

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44

Padova, C. Non-reacting mixing components: Final report for the period November 1979 to August 1985. Buffalo, N.Y: Calspan Advanced Technology Center, 1985.

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45

O, Demuren A., i United States. National Aeronautics and Space Administration., red. Computations of complex three-dimensional turbulent free jets. Norfolk, Va: Institute for Computational and Applied Mechanics, Old Dominion University, 1997.

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46

J, Morris Philip, i United States. National Aeronautics and Space Administration., red. Supersonic coaxial jet noise predictions. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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47

Nallasamy, M. Prediction of recirculation zones in isothermal coaxial jet flows relevant to combustors. Huntsville, Ala: Marshall Space Flight Center, 1987.

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48

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Prediction of recirculation zones in isothermal coaxial jet flows relevant to combustors. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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49

Simon, Frederick F. Jet model for slot film cooling with effect of free-stream and coolant turbulence. Cleveland, Ohio: Lewis Research Center, 1986.

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50

University, Arizona State, i Langley Research Center, red. Near-wall modelling of compressible turbulent flows: A semi-annual progress report. Tempe, Ariz: Arizona State University, 1990.

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