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1

Smits, Alexander J. Turbulent shear layers in supersonic flow. 2nd ed. New York: Springer, 2011.

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2

Jean-Paul, Dussauge, ed. Turbulent shear layers in supersonic flow. 2nd ed. New York: Springer, 2006.

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3

Jean-Paul, Dussauge, ed. Turbulent shear layers in supersonic flow. Woodbury, N.Y: American Institute of Physics, 1996.

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4

Papamoschou, Dimitri. Structure of the compressible turbulent shear layer. Washington, D. C: American Institute of Aeronautics and Astronautics, 1989.

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5

Y, Chen J., Limley J. L, and Lewis Research Center. Institute for Computational Mechanics in Propulsion., eds. 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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6

Shau, Y. R. Experimental study of spreading rate enhancement of high Mach number turbulent shear layers. Washington, D. C: American Institute of Aeronautics and Astronautics, 1989.

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7

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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8

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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9

Adair, Desmond. Characteristics of merging shear layers and turbulent wakes of a multi-element airfoil. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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10

Brown, Douglas L. Computation of turbulent boundary layers employing the defect wall-function method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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11

C, Dudek Julianne, Tierney Thomas P, and United States. National Aeronautics and Space Administration., eds. Grid resolution and turbulent inflow boundary condition recommendations for NPARC calculations. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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12

F, Durst, and International Symposium on Turbulent Shear Flows, (9th : 1993 : Kyoto, Japan), eds. Turbulent shear flows 9: Selected papers from the Ninth International Symposium on Turbulent Shear Flows, Kyoto, Japan, August 16-18, 1993. Berlin: Springer-Verlag, 1995.

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13

University), International Symposium on Turbulent Shear Flows (7th 1989 Stanford. Turbulent shear flows 7: Selected papers from the Seventh International Symposium on Turbulent Shear Flows, Stanford University, USA, August 21-23, 1989. Berlin: Springer-Verlag, 1991.

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14

Délery, J., ed. Turbulent Shear-Layer/Shock-Wave Interactions. Berlin, Heidelberg: Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-82770-9.

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15

IUTAM Symposium (1985 Palaiseau, France). Turbulent shear-layer/shock-wave interactions. Edited by Délery J. 1939-, International Union of Theoretical and Applied Mechanics., and France. Office national d'études et de recherches aérospatiales. Berlin: Springer-Verlag, 1986.

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16

International Symposium on Turbulent Shear Flows (5th 1985 Cornell University, Ithaca, N.Y.). Turbulent shear flows: Papers from the Fifth International Symposium on Turbulent Shear Flows, August 7-9, 1985, Cornell University, Ithaca, NY. [University Park, Pa: Pennsylvania State University, 1985.

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17

Woppowa, Stefan. Über Gedächtniseffekte in der Turbulenz. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1993.

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18

American Society of Mechanical Engineers. Winter Meeting. Shear flow: Structure interaction phenomena. New York, N.Y. (345 E. 47th St., New York): American Society of Mechanical Engineers, 1985.

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19

Kim, S. W. Calculation of reattaching shear layers in divergent channel with a multiple-time-scale turbulence model. Cleveland, Ohio: Institute for Computational Mechanics in Propulusion, 1989.

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20

B, Gatski T., and Langley Research Center, eds. An alternative assessment of second order closure models in turbulent shear flows. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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21

Driver, David M. Experimental study of a three-dimensional shear-driven turbulent boundary layer with streamwise adverse pressure gradient. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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22

United States. National Aeronautics and Space Administration., ed. Turbulence modeling of free shear layers for high performance aircraft. San Jose, CA: MCAT Institute, 1993.

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23

United States. National Aeronautics and Space Administration., ed. Turbulence modeling of free shear layers for high performance aircraft. San Jose, CA: MCAT Institute, 1993.

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24

United States. National Aeronautics and Space Administration., ed. Turbulence modeling of free shear layers for high-performance aircraft. San Jose, CA: MCAT Institute, 1993.

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25

International Symposium on Turbulent Shear Flows (9th 1993 Kyoto, Japan). Turbulent shear flows 9: Selected papers from the Ninth International Symposium on Turbulent Shear Flows, Kyoto, Japan, August 16-18, 1993. Edited by Durst F. Berlin: Springer-Verlag, 1995.

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26

International Symposium on Turbulent Shear Flows (8th 1991 Munich, Germany). Turbulent shear flows 8: Selected papers from the Eighth International Symposium on Turbulent Shear Flows, Munich, FRG, September 9-11, 1991. Edited by Durst F. Berlin: Springer-Verlag, 1993.

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27

L, Bowles Roland, and Langley Research Center, eds. A simple, analytic 3-dimensional downburst model based on boundary layer stagnation flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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28

L, Bowles Roland, and Langley Research Center, eds. A simple, analytic 3-dimensional downburst model based on boundary layer stagnation flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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29

G, Huang P., MacInnes J. M, and United States. National Aeronautics and Space Administration., eds. Mesh refinement in a two-dimensional large eddy simulation of a forced shear layer. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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30

Sarkar, Sutanu. Application of a Reynolds stress turbulence model to the compressible shear layer. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

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31

Driver, David M. Experimental study of a three-dimensional, shear-driven, turbulent boundary layer using a three-dimensional laser doppler velocimeter. [New York]: American Institute of Aeronautics and Astronautics, 1985.

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32

Délery, J. Turbulent Shear-Layer/Shock-Wave Interactions: IUTAM Symposium, Palaiseau, France September 9-12, 1985. Berlin, Heidelberg: Springer Berlin Heidelberg, 1986.

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33

Sarkar, Sarben. Application of a Reynolds stress turbulence model to the compressible shear layer. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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34

IUTAM Symposium (1993 Potsdam, N.Y.). Nonlinear instability of nonparallel flows. Berlin: Springer-Verlag, 1994.

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35

United States. National Aeronautics and Space Administration., ed. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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36

United States. National Aeronautics and Space Administration., ed. Low re multiple-time-scale turbulence model and calculations of steady and pulsating shear layers. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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37

M, Abbott John, and United States. National Aeronautics and Space Administration., eds. Control of flow separation and mixing by aerodynamic excitation. [Washington, D.C.]: NASA, 1990.

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38

M, Abbott John, and United States. National Aeronautics and Space Administration., eds. Control of flow separation and mixing by aerodynamic excitation. [Washington, D.C.]: NASA, 1990.

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39

C, Yee H., and Research Institute for Advanced Computer Science (U.S.), eds. Performance of low dissipative high order shock-capturing schemes for shock-turbulence interactions. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1998.

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40

Kline, Stephen. The physics of turbulence in the boundary layer: Final report ... NASA grant NAG-1-1610. [Washington, DC: National Aeronautics and Space Administration, 1996.

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41

Clawson, K. L. Meteorological measurements during the urban 2000/VTMX field study. Silver Spring, Md: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Oceanic and Atmospheric Research Laboratories, Air Resources Laboratory, 2002.

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42

T, Chang C., and United States. National Aeronautics and Space Administration., eds. Turbulence measurement in a reacting and non-reacting shear layer at a high subsonic Mach number. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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43

T, Chang C., and United States. National Aeronautics and Space Administration., eds. Turbulence measurement in a reacting and non-reacting shear layer at a high subsonic Mach number. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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44

Kamada, Ray. Amending the w* velocity scale for surface layer, entrainment zone, and baroclinic shear in mixed forced/free turbulent convection. Monterey, Calif: Naval Postgraduate School, 1992.

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45

Dahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

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46

Dahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

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47

J, Morris P., and United States. National Aeronautics and Space Administration., eds. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

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48

Dahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

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49

Dahl, M. D. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

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50

J, Morris P., and United States. National Aeronautics and Space Administration., eds. Noise from supersonic coaxial jets. [Washington, DC: National Aeronautics and Space Administration, 1997.

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