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1

Center, Langley Research, ed. Optimum suction distribution for transition control. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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2

Center, Langley Research, ed. Optimum suction distribution for transition control. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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3

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., ed. A numerical study of transition control by periodic suction-blowing. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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4

Smith, A. Instability and transition of flow at, and near, an attachment-line: Including control by surface suction. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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5

A, Poll D. I., and United States. National Aeronautics and Space Administration., eds. Instability and transition of flow at, and near, an attachment-line: Including control by surface suction : contract number NCC1-218. [Washington, DC: National Aeronautics and Space Administration, 1996.

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6

1945-, Gad-el-Hak Mohamed, and Tsai Her Mann, eds. Transition and turbulence control. New Jersey: World Scientific, 2006.

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7

United States. National Aeronautics and Space Administration., ed. Instabilities originating from suction holes used for laminar flow control (LFC). [Washington, DC: National Aeronautics and Space Administration, 1994.

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8

Kozarzewski, Piotr. State Corporate Control in Transition. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-78562-8.

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9

International Erosion Control Association. Conference. Erosion control: Technology in transition. Steamboat Springs, CO: International Erosion Control Association, 1990.

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10

author, Dong Gang 1970, ed. Principles of turbulence control. Singapore: John Wiley & Sons, 2015.

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11

Braslow, Albert L. A history of suction-type laminar-flow control with emphasis on flight research. Washington, DC: NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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12

Braslow, Albert L. A history of suction-type laminar-flow control with emphasis on flight research. Washington, DC: NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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13

Braslow, Albert L. A history of suction-type laminar-flow control with emphasis on flight research. Washington, DC: NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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14

Braslow, Albert L. A history of suction-type laminar-flow control with emphasis on flight research. Washington, DC: NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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15

Braslow, Albert L. A history of suction-type laminar-flow control with emphasis on flight research. Washington, DC: NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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16

Braslow, Albert L. A history of suction-type laminar-flow control with emphasis on flight research. Washington, DC: NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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17

Braslow, Albert L. A history of suction-type laminar-flow control with emphasis on flight research. Washington, DC: NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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18

Braslow, Albert L. A history of suction-type laminar-flow control with emphasis on flight research. Washington, DC: NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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19

Analytical Services & Materials, Inc. and Langley Research Center, eds. Effect of suction on controlling the secondary instability of boundary layers. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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20

Maddalon, Dal V. Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system. Hampton, Va: Langley Research Center, 1990.

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21

L, Braslow Albert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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22

W, Duck Peter, and Langley Research Center, eds. Boundary-layer receptivity due to a wall suction and control of Tollmein-Schlichting waves. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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23

Bodonyi, R. J. Boundary-layer receptivity due to a wall suction and control of Tollmien-Schlichting waves. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

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24

W, Duck Peter, and Langley Research Center, eds. Boundary-layer receptivity due to a wall suction and control of Tollmein-Schlichting waves. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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25

Brooks, Cuyler W. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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26

Brooks, Cuyler W. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. Hampton, Va: Langley Research Center, 1991.

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27

Brooks, Cuyler W. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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28

Braslow, Albert L. A history of suction-type laminar-flow control with empahsis [i.e. emphasis] on flight research. Washington, D.C: NASA History Division, Office of Policy and Plans, NASA Headquarters, 1999.

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29

1952-, Harris Charles D., Harvey William D. 1934-, United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., and Langley Research Center, eds. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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30

Brooks, Cuyler W. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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31

Braslow, Albert L. A history of suction-type laminar-flow control with empahsis [i.e. emphasis] on flight research. Washington, D.C: NASA History Division, Office of Policy and Plans, NASA Headquarters, 1999.

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32

Frost & Sullivan., ed. Medical and dental suction and irrigation equipment markets: Environmental and infection control issues encourage innovation. Mountain View, CA: Frost & Sullivan, Inc., 1993.

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33

United States. National Aeronautics and Space Administration., ed. Effects of suction on swept-wing transition: Final technical report on NASA-Langley award # NAG-1-194, 16 December 1995 to 31 March 1998. [Washington, DC: National Aeronautics and Space Administration, 1998.

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34

Castro, Rafael Fernández de, and Andrew D. Selee. Mexico in transition. Washington, D.C: Woodrow Wilson International Center for Scholars, Latin American Program, 2001.

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35

Freedman, Ronald. Observing Taiwan's demographic transition: A memoir. Taichung, Taiwan, R.O.C: Taiwan Provincial Institute of Family Planning, 1998.

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36

Freedman, Ronald. Observing Taiwan's demographic transition: A memoir. Taichung, Taiwan, R.O.C: Taiwan Provincial Institute of Family Planning, 1998.

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37

United States. National Aeronautics and Space Administration., ed. Numerical simulation of receptivity and transition in a boundary layer on a flat plate with a suction hole. Tucson, Ariz: Engineering Experiment Station College of Engineering and Mines, University of Arizona, 1994.

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38

United States. National Aeronautics and Space Administration., ed. Numerical simulation of receptivity and transition in a boundary layer on a flat plate with a suction hole. Tucson, Ariz: Engineering Experiment Station College of Engineering and Mines, University of Arizona, 1994.

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39

Westoff, Charles F. The stall in the fertility transition in Kenya. Calverton, MD: ORC Macro, 2006.

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40

Banks, Cyndi. Women in transition: Social control in Papua New Guinea. Canberra, ACT: Australian Institute of Criminology, 1993.

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41

McKinnon, Ronald I. Financial control in the transition to a market economy. London: Centre for Economic Performance, 1991.

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42

Consulting, ABS. ISO 9001: 2000 transition workbook. Rockville, Md: ABS Consulting, 2002.

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43

Shariff, Abusaleh. Fertility transition in rural South India. New Delhi: Gian Pub. House, 1989.

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44

B, Gilyard Glenn, Myers Lawrence P, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Propulsion system/flight control integration and optimization: Flight evaluation and technology transition. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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45

F, Borchers Paul, and Ames Research Center, eds. YAV-8B reaction control system bleed and control power usage in hover and transition. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

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46

F, Borchers Paul, and Ames Research Center, eds. YAV-8B reaction control system bleed and control power usage in hover and transition. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

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47

F, Borchers Paul, and Ames Research Center, eds. YAV-8B reaction control system bleed and control power usage in hover and transition. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

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48

F, Borchers Paul, and Ames Research Center, eds. YAV-8B reaction control system bleed and control power usage in hover and transition. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

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49

Sandron, Frédéric. La transition de la fécondité en Tunisie. Paris: L'Harmattan, 2002.

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50

Sandron, Frédéric. La transition de la fécondité en Tunisie. Paris: Harmattan, 2002.

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