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1

Wilson, Miles. Mathematical modelling of bubble-vortex interactions. Birmingham: University of Birmingham, 1997.

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2

Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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3

Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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4

Srinivasan, G. Computations of two-dimensional airfoil-vortex interactions. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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5

Srinivasan, G. Computations of two-dimensional airfoil-vortex interactions. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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6

Jackson, Thomas L. Role of acoustics in flame/vortex interactions. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1993.

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7

Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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8

Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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9

Hall, Philip. On the initial stages of vortex wave interactions in highly curved boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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10

Hall, Philip. On the initial stages of vortex wave interactions in highly curved boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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11

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1993.

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12

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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13

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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14

Blackaby, Nicholas D. Tollmien-Schlichting/vortex interactions in compressible boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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15

Martin, R. M. Advancing-side directivity and retreating-side interactions of model rotor blade-vortex interaction noise. Hampton, Va: Langley Research Center, 1987.

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16

Hall, Philip. On strongly nonlinear vortex/wave interactions in boundary-layer transition. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1989.

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17

Bradshaw, P. Vortex boundary-layer interactions, data report: Semiannual status report on research grant no. NAGW-581, period 1 March 1985 - 31 August 1985. London: Imperial College of Science and Technology, Department of Technology, 1985.

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18

Neubert, Donald E. Trailing vortex free-surface interaction. Monterey, Calif: Naval Postgraduate School, 1992.

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19

Hofert, Glenn D. Spectral analysis of vortex/free-surface interaction. Monterey, Calif: Naval Postgraduate School, 1994.

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20

Bertolotti, Fabio P. Vortex generation and wave-vortex interaction over a concave plate with roughness and suction. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1993.

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21

Erlebacher, Gordon. Interaction of a shock with a longitudinal vortex. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1996.

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22

Hall, Philip. Nonlinear Tollmien-Schlichting/vortex interaction in boundary layers. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1988.

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23

Ribner, Herbert S. Cylindrical sound wave generated by shock-vortex interaction. [S.l.]: [s.n.], 1985.

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24

Hall, Philip. Nonlinear Tollmien-Schlichting/vortex interaction in boundary layers. Hampton, Va: ICASE, 1988.

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25

Hall, Philip. Nonlinear Tollmien-Schlichting/vortex interaction in boundary layers. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1988.

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26

Merrill, Craig F. Numerical analysis of single-vortex/free-surface interaction. Monterey, Calif: Naval Postgraduate School, 1993.

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27

Hall, Philip. Nonlinear Tollmien-Schlichting/vortex interaction in boundary layers. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1988.

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28

Vortex flow in nature and technology. Malabar, Fla: Krieger, 1995.

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29

Westphal, R. V. Interaction between a vortex and a turbulent boundary layer. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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30

Wang, Clin N. Numerical vorticity capturing for vortex-solid body interaction problems. Washington, D. C: American Institute of Aeronautics and Astronautics, 1993.

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31

Martin, R. M. Wake geometry effects on rotor blade-vortex interaction noise directivity. Hampton, Va: Langley Research Center, 1990.

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32

Smith, Brian E. Application of a panel method to wake-vortex/wing interaction and comparison with experimental data. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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33

G, Macaraeg Michele, Hussaini M. Yousuff, and Langley Research Center, eds. Role of acoustics in flame/vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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34

Center, Langley Research, ed. Full-potential modeling of blade-vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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35

Full-potential modeling of blade-vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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36

Full-potential modeling of blade-vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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37

Center, Langley Research, ed. Full-potential modeling of blade-vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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38

Y, Xue, and United States. National Aeronautics and Space Administration., eds. Transonic blade-vortex interactions noise: A parametric study. Minneapolis, Minn: Aerospace Engineering & Mechanics, University of Minnesota, 1991.

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39

Y, Xue, and United States. National Aeronautics and Space Administration., eds. Transonic blade-vortex interactions noise: A parametric study. Minneapolis, Minn: Aerospace Engineering & Mechanics, University of Minnesota, 1991.

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40

1956-, Martin R. M., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Advancing-side directivity and retreating-side interactions of model rotor blade-vortex interaction noise. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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41

1956-, Martin R. M., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Advancing-side directivity and retreating-side interactions of model rotor blade-vortex interaction noise. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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42

1948-, Smith F. T., and Langley Research Center, eds. On strongly nonlinear vortex/wave interactions in boundary-layer transition. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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43

A study of the noise mechanisms of transonic blade-vortex interactions. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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44

1935-, Bradshaw P., and United States. National Aeronautics and Space Administration., eds. Vortex/boundary-layer interactions, data report: Final report on NASA grant NAGw-581. London: Imperial College of Science and Technology, Dept. of Technology, 1988.

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45

1935-, Bradshaw P., and United States. National Aeronautics and Space Administration., eds. Vortex/boundary-layer interactions, data report: Final report on NASA grant NAGw-581. London: Imperial College of Science and Technology, Dept. of Technology, 1988.

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46

A weakly nonlinear theory for wave-vortex interactions in curved channel flow. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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47

1935-, Bradshaw P., and United States. National Aeronautics and Space Administration., eds. Vortex/boundary-layer interactions, data report: Final report on NASA grant NAGw-581 / A.D. Cutler and P. Bradshaw. London: Imperial College of Science and Technology, Department of Aeronautics, 1988.

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48

Vortex/boundary-layer interactions, data report: Final report on NASA grant NAGw-581 / A.D. Cutler and P. Bradshaw. London: Imperial College of Science and Technology, Department of Aeronautics, 1988.

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49

(Editor), M. Brocchini, and F. Trivellato (Editor), eds. Vorticity And Turbulence Effects in Fluid Structure Interactions: An Application to Hydraulic Structure Design (Advances in Fluid Mechanics). WIT Press (UK), 2006.

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50

Center, Ames Research, ed. Transonic Navier-Stokes computations of strake-generated vortex interactions for a fighter-like configuration. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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