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1

Ajay, Kumar, Kegelman Jerome T, and United States. National Aeronautics and Space Administration., eds. The Langley wind tunnel enterprise. [Washington, DC: National Aeronautics and Space Administration, 1998.

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2

Ajay, Kumar, Kegelman Jerome T, and United States. National Aeronautics and Space Administration., eds. The Langley wind tunnel enterprise. [Washington, DC: National Aeronautics and Space Administration, 1998.

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3

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. Neuilly-sur-Seine, France: AGARD, 1994.

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4

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. Neuilly-sur-Seine: AGARD, 1994.

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5

MacKinnon, A. Wind tunnel tests on a variable camber wing. Cranfield, Bedford, England: College of Aeronautics, Cranfield University, 1993.

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6

Galway, R. D. The IAR High Reynolds Number Two-Dimensional Test Facility - a description of equipment and procedures common to most 2-D airfoil tests. Ottawa, Ont: National Research Council Canada, Institute for Aerospace Research, 1990.

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7

Galway, R. D. The IAR high Reynolds number two-dimensional test facility - a description of equipment and procedures common to most 2-D airfoil tests. Ottawa: National Research Council of Canada, Institute for Aerospace Research, 1990.

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8

Center, Lewis Research, and United States. National Aeronautics and Space Administration., eds. Flow field surveys of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1993 test). [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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9

Kelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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10

Kelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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11

K, Abeyounis W., and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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12

A, Kilgore Robert, Moore Deborah L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Cryogenic wind tunnels: A comprehensive, annotated bibliography. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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13

A, Kilgore Robert, Cole Karen L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Cryogenic wind tunnels: A selected, annotated bibliography. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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14

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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15

Britcher, Colin P. Applications of magnetic suspension technology to large scale facilities: Progress, problems and promises. [Washington, DC: National Aeronautics and Space Administration, 1997.

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16

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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17

Britcher, Colin P. Application of magnetic suspension and balance systems to ultra-high Reynolds number facilities. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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18

A, Laub James, and Ames Research Center, eds. NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.

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19

Mabey, Dennis G. Further buffeting tests in a cryogenic wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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20

Mabey, D. G. Further buffeting tests in a cryogenic wind tunnel. London: HMSO, 1991.

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21

R, Curry Monroe, Arrington E. Allen, United States. National Aeronautics and Space Administration., NASA Glenn Research Center, American Institute of Aeronautics and Astronautics., and Aerospace Sciences Meeting & Exhibit (39th : 2001 : Reno, Nev.), eds. Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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22

R, Curry Monroe, Arrington E. Allen, United Stares. National Aeronautics and Space Administration., NASA Glenn Research Center, American Institute of Aeronautics and Astronautics., and Aerospace Sciences Meeting & Exhibit (39th : 2001 : Reno, Nev.), eds. Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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23

R, Curry Monroe, Arrington E. Allen, United Stares. National Aeronautics and Space Administration., NASA Glenn Research Center, American Institute of Aeronautics and Astronautics., and Aerospace Sciences Meeting & Exhibit (39th : 2001 : Reno, Nev.), eds. Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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24

R, Curry Monroe, Arrington E. Allen, United States. National Aeronautics and Space Administration., NASA Glenn Research Center, American Institute of Aeronautics and Astronautics., and Aerospace Sciences Meeting & Exhibit (39th : 2001 : Reno, Nev.), eds. Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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25

Baumeister, Kenneth J. Reverberation effects on directionality and response of stationary monopole and dipole sources in a wind tunnel. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

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26

Center, Langley Research, ed. A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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27

Center, Langley Research, ed. A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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28

Center, Langley Research, ed. A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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29

Buttrill, Carey S. Aeroservoelastic simulation of an active flexible wing wind tunnel model. Hampton, Va: Langely Research Center, 1996.

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30

A, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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31

A, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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32

A, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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33

A, Houck Jacob, and Langley Research Center, eds. Hot-bench simulation of the active flexible wing wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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34

Mineck, Raymond E. Wind-tunnel investigation of aerodynamic efficiency of three planar elliptical wings with curvature of quarter-chord line. Hampton, Va: Langley Research Center, 1993.

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35

Mirick, Paul H. Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing. Hampton, Va: Langley Research Center, 1990.

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36

Allen, Kilgore W., and Langley Research Center, eds. Microcomputer based controller for the Langley 0.3-meter Transonic Cryogenic Tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

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37

T, Lund, Rote Donald, and Langley Research Center, eds. High-lift flight tunnel: Phase II report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

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38

T, Lund, Rote Donald, and Langley Research Center, eds. High-lift flight tunnel: Phase II report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

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39

Rizkalla, Oussama F. High pressure hypervelocity electrothermal wind tunnel performance study and subscale tests. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.

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40

Newton, James E. Study of ice accretion on icing wind tunnel components. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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41

Larson, Terry J. Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

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42

R, Moes Timothy, Siemers Paul M, and Dryden Flight Research Facility, eds. Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

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43

Wieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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44

Wieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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45

Wieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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46

Wieseman, Carol D. On-line analysis capabilities developed to support the AFW wind-tunnel tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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47

Allen, Arrington E., American Institute of Aeronautics and Astronautics., NASA Glenn Research Center, and Aerospace Sciences Meeting & Exhibit (36th : 1998 : Reno, Nev.), eds. Aerodynamic calibration of the NASA Lewis icing research tunnel (1997 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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48

Center, Langley Research, and United States. National Aeronautics and Space Administration, eds. Aeroservoelastic testing of free flying wind tunnel models. Hampton, Virginia: National Aeronautics and Space Administration, Langley Research Center, 2013.

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49

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Wall interference, support interference and flow field measurements. Neuilly sur Seine, France: AGARD, 1994.

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50

Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium,, ed. Wall interference, support interference and flow field measurements: Papers presented and discussions recorded at the 73rd Fluid Dynamics Panel Symposium held in Brussels, Belgium, 4th-7th October 1993. Neuilly sur Seine: Agard, 1994.

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