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1

Chang, Paul K. Recent development in flow separation. Pang Han Pub. Co., 1985.

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2

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

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3

G, Allan Brian, and Institute for Computer Applications in Science and Engineering., eds. Closed-loop separation control using oscillatory flow excitation. ICASE, National Aeronautics and Science Administration, Langley Research Center, 2000.

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4

G, Allan Brian, and Institute for Computer Applications in Science and Engineering., eds. Closed-loop separation control using oscillatory flow excitation. ICASE, National Aeronautics and Science Administration, Langley Research Center, 2000.

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5

G, Allan Brian, Institute for Computer Applications in Science and Engineering., and Langley Research Center, eds. Closed-loop separation control using oscillatory flow excitation. Institute for Computer Applications in Science and Engineering, Langley Research Center, 2000.

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6

Ravindran, S. S. Active control of flow separation over an airfoil. National Aeronautics and Space Administration, Langley Research Center, 1999.

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7

Ravindran, S. S. Active control of flow separation over an airfoil. National Aeronautics and Space Administration, Langley Research Center, 1999.

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8

M, Abbott John, and United States. National Aeronautics and Space Administration., eds. Control of flow separation and mixing by aerodynamic excitation. NASA, 1990.

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9

M, Abbott John, and United States. National Aeronautics and Space Administration., eds. Control of flow separation and mixing by aerodynamic excitation. NASA, 1990.

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10

Dovgal, Alexander. Control of leading-edge separation on an airfoil by localized excitation. DLR, 1993.

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11

Old Dominion University. Research Foundation. and Langley Research Center, eds. Experimental parametric study of jet vortex generators for flow separation control. Old Dominion University Research Foundation, 1991.

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12

Qin, Ning, Jacques Periaux, and Gabriel Bugeda, eds. Advances in Effective Flow Separation Control for Aircraft Drag Reduction. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-29688-9.

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13

Center, NASA Glenn Research, ed. Low-pressure turbine separation control: Comparison with experimental data. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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14

Center, NASA Glenn Research, ed. Low-pressure turbine separation control: Comparison with experimental data. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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15

E, Ashpis D., and NASA Glenn Research Center, eds. Demonstration of separation delay with glow-discharge plasma actuators. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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16

E, Ashpis D., and NASA Glenn Research Center, eds. Demonstration of separation delay with glow-discharge plasma actuators. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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17

Corke, Thomas C. Enhanced design of turbo-jet LPT by separation control using phased plasma actuators. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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18

Corke, Thomas C. Enhanced design of turbo-jet LPT by separation control using phased plasma actuators. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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19

Corke, Thomas C. Enhanced design of turbo-jet LPT by separation control using phased plasma actuators. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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20

United States. Environmental Protection Agency. Office of Water. Municipal Technology Branch and National Risk Management Research Laboratory (U.S.). Urban Watershed Management Branch, eds. Assessment of vortex solids separators for the control and treatment of wet-weather flow. U.S. Environmental Protection Agency, Office of Wastewater Management, Municipal Support Division, Municipal Technology Branch, 1996.

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21

United States. Environmental Protection Agency. Office of Water. Municipal Technology Branch. and National Risk Management Research Laboratory (U.S.). Urban Watershed Management Branch., eds. Assessment of vortex solids separators for the control and treatment of wet-weather flow. U.S. Environmental Protection Agency, Office of Wastewater Management, Municipal Support Division, Municipal Technology Branch, 1996.

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22

United States. National Aeronautics and Space Administration., ed. Control of low-speed turbulent separated flow over a backward-facing ramp. National Aeronautics and Space Administration, 1994.

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23

United States. National Aeronautics and Space Administration., ed. Control of low-speed turbulent separated flow over a backward-facing ramp. National Aeronautics and Space Administration, 1994.

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24

United States. National Aeronautics and Space Administration., ed. Control of low-speed turbulent separated flow over a backward-facing ramp. National Aeronautics and Space Administration, 1994.

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25

Forum on Unsteady Flow Separation (1987 Cincinnati, Ohio). Forum on Unsteady Flow Separation: Presented at the 1987 ASME Applied Mechanics, Bioengineering, and Fluids Engineering Conference, Cincinnati, Ohio, June 14-17, 1987. American Society of Mechanical Engineers, 1987.

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26

United States. National Aeronautics and Space Administration., ed. Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil. Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, 1996.

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27

United States. National Aeronautics and Space Administration., ed. Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil. Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center, 1996.

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28

United States. National Aeronautics and Space Administration., ed. Control of unsteady separated flow associated with the dynamic stall of airfoils. MCAT Institute, 1994.

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29

Saeed, Farokhi, and United States. National Aeronautics and Space Administration., eds. A study of three dimensional turbulent boundary layer separation and vortex flow control using the reduced Navier Stokes equations. National Aeronautics and Space Administration, 1991.

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30

United States. National Aeronautics and Space Administration., ed. Control of unsteady separated flow associated with the dynamic stall of airfoils: Final report, 95-09. MCAT Institute, 1995.

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31

W, Barter J., and United States. National Aeronautics and Space Administration., eds. Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction: Final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95. Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin, 1995.

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32

W, Barter J., and United States. National Aeronautics and Space Administration., eds. Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction: Final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95. Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin, 1995.

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33

W, Barter J., and United States. National Aeronautics and Space Administration., eds. Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction: Final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95. Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin, 1995.

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34

Bebchuk, Lucian A. Stock pyramids, cross-ownership, and dual class equity: The creation and agency costs of separating control from cash flow rights. National Bureau of Economic Research, 1999.

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35

Closed-loop separation control using oscillatory flow excitation. ICASE, National Aeronautics and Science Administration, Langley Research Center, 2000.

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36

National Aeronautics and Space Administration (NASA) Staff. Active Control of Flow Separation over an Airfoil. Independently Published, 2018.

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37

National Aeronautics and Space Administration (NASA) Staff. Closed-Loop Separation Control Using Oscillatory Flow Excitation. Independently Published, 2018.

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38

Hustvedt, Eric L. Control of a continuous flow centrifuge to study cell separations. 1985.

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39

Low-pressure turbine separation control: Comparison with experimental data. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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40

Low-pressure turbine separation control: Comparison with experimental data. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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41

Periaux, Jacques, Ning Qin, and Gabriel Bugeda. Advances in Effective Flow Separation Control for Aircraft Drag Reduction: Modeling, Simulations and Experimentations. Springer, 2019.

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42

Periaux, Jacques, Ning Qin, and Gabriel Bugeda. Advances in Effective Flow Separation Control for Aircraft Drag Reduction: Modeling, Simulations and Experimentations. Springer International Publishing AG, 2020.

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43

Transient growth theory prediction of optimal placing of passive and active flow control devices for separation delay in LPT airfoils. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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44

Control of low-speed turbulent separated flow over a backward-facing ramp. National Aeronautics and Space Administration, 1994.

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45

Control of unsteady separated flow associated with the dynamic stall of airfoils. MCAT Institute, 1992.

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46

Ives, K. J. Control of Organic Material by Coagulation and Floc-Separation Processes. Elsevier Science Pub Co, 1993.

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47

Komaitis, Konstantinos. The Democratic Nature of the Internet’s Infrastructure. International Institute for Democracy and Electoral Assistance (International IDEA), 2023. http://dx.doi.org/10.31752/idea.2023.35.

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The strength of the Internet lies in its original design, which in some ways mirrors democratic ideas. As with the separation of powers in a true democratic state, the architecture of the Internet has no centre of control and allows power to flow from the bottom up and even from the margins, rather than always from above. During the past few years, policymakers have directed their attention towards the top layers of the ‘Internet stack’, those where the effect on democracy is more easily observable. Little attention has been paid to the infrastructure of the Internet—the part that is invisible
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