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1

Barlow, Jewel B. Low-speed wind tunnel testing. 3rd ed. New York: Wiley, 1999.

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2

Bell, James H. Contraction design for small low-speed wind tunnels. Stanford, Calif: Stanford University, Department of Aeronautics and Astronautics, 1988.

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3

S, Walker Betty, Millard Betty F, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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4

United States. National Aeronautics and Space Administration., ed. Integral method of wall interference correction in low-speed wind tunnels. Washington, DC: National Aeronautics and Space Administration, 1987.

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5

Watmuff, J. H. Design of a new contraction for the ARL low speed wind tunnel (U). Melbourne, Australia: Aeronautical Research Laboratories, 1986.

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6

United States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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7

United States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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8

United States. National Aeronautics and Space Administration., ed. NASA Lewis 9-by 15-foot low-speed wind tunnel user manual. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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9

Bell, J. H. Contraction design for small low-speed wind tunnels. [Washington, DC: National Aeronautics and Space Administration, 1988.

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10

J, Engebretson M., Takahashi K, and Scholer M. 1940-, eds. Solar wind sources of magnetospheric ultra-low-frequency waves. Washington, DC, USA: American Geophysical Union, 1994.

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11

Shepherd, Kevin P. Detection of low frequency impulsive noise from large wind turbine generators. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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12

Goodyer, M. J. Introduction to cryogenic wind tunnels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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13

T, Steinberg J., McNutt Ralph L, and United States. National Aeronautics and Space Administration., eds. A low-mass Faraday Cup experiment for the solar wind. [Washington, DC: National Aeronautics and Space Administration, 1993.

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14

T, Steinberg J., McNutt Ralph L, and United States. National Aeronautics and Space Administration., eds. A low-mass Faraday Cup experiment for the solar wind. [Washington, DC: National Aeronautics and Space Administration, 1993.

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15

Engebretson, M. J., K. Takahashi, and M. Scholer, eds. Solar Wind Sources of Magnetospheric Ultra-Low-Frequency Waves. Washington, D. C.: American Geophysical Union, 1994. http://dx.doi.org/10.1029/gm081.

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16

Leeuwen, P. J. van. Low frequency wave generation due to breaking wind waves. [Delft]: Faculty of Civil Engineering, Delft University of Technology, 1992.

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17

Midden, Raymond E. Description and calibration of the Langley hypersonic CF: A facility for simulating low. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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18

Midden, Raymond E. Description and calibration of the Langley hypersonic CF: A facility for simulating low ©. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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19

T, Pickett Mark, and United States. National Aeronautics and Space Administration., eds. Flow quality studies of the NASA Lewis Research Center 8- by 6-foot supersonic/9- by 15-foot low speed wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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20

Goodyer, M. J. A swept wing panel in a low speed flexible walled test section. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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21

Goodyer, M. J. A swept wing panel in a low speed flexible walled test section. Hampton, Va: Langley Research Center, 1987.

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22

K, Brown Christopher, and Langley Research Center, eds. Computational design of low aspect ratio wing-winglet configurations for transonic wind-tunnel tests. Morgantown, WV: Mechanical and Aerospace Engineering Dept., West Virginia University, 1988.

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23

H, Harris Scott, and Ames Research Center, eds. Computation of wind tunnel wall effects for complex models using a low-order panel method. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

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24

United States. National Aeronautics and Space Administration., ed. Cryogenic wind tunnels: Problems of continuous operation at low temperatures. Washington DC: National Aeronautics and Space Administration, 1986.

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25

Gobert, J. Preliminary study of an apparatus to control the temperature of the flow entering the T2 cryogenic wind tunnel. Washington, DC: National Aeronautics and Space Administration, 1987.

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26

T, Pickett Mark, Soeder Ronald H, and United States. National Aeronautics and Space Administration., eds. Calibration of NASA Lewis Research Center 9- by 15-Foot low speed wind tunnel (1992 text). [Washington, DC]: National Aeronautics and Space Administration, 1996.

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27

Bowcutt, K. G. The use of panel methods for the development of low subsonic wall interference and blockage corrections. New York: AIAA, 1985.

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28

Khadjavi, F. Two-dimensional test section with preadjusted adaptive walls for low speed wind tunnel. Stockholm: Royal Institute of Technology, Department of Aeronautics, 1987.

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29

Jordan, J. R. Feasibility study for a low-altitude wind and temperature profiler. Boulder, Colo: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Wave Propagation Laboratory, 1992.

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30

E, Hahne David, Cockrell Charles E, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel tests of two waverider configuration models. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

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31

E, Hahne David, Cockrell Charles E, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel tests of two waverider configuration models. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

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32

P, Woodward Richard, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Acoustical evaluation of the NASA Lewis 9- by 15-foot low speed wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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33

P, Woodward Richard, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Acoustical evaluation of the NASA Lewis 9- by 15-foot low speed wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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34

A, Mignosi, Plazanet M, and United States. National Aeronautics and Space Administration., eds. Qualification of the T2 wind tunnel in cryogenic operation. Washington DC: National Aeronautics and Space Administration, 1985.

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35

V, Delcourt, Plazanet M, and United States. National Aeronautics and Space Administration., eds. Problems associated with operations and measurement in cryogenic wind tunnels. Washington DC: National Aeronautics and Space Administration, 1986.

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36

V, Delcourt, Plazanet M, and United States. National Aeronautics and Space Administration., eds. Problems associated with operations and measurement in cryogenic wind tunnels. Washington DC: National Aeronautics and Space Administration, 1986.

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37

Center, Langley Research, ed. Low speed wind tunnel test of a propulsive wing/canard concept in the STOL configuration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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38

A, Kilgore Robert, McGuire Peggy D, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, eds. Cryogenic wind tunnels: A selected, annotated bibliography. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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39

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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40

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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41

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Spectrum modal analysis for the detection of low-altitude windshear with airborne Doppler radar. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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42

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Spectrum modal analysis for the detection of low-altitude indshear with airborne Doppler radar. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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43

Dunham, Dana Morris. Low-speed wind-tunnel tests of single- and counter-rotation propellers. [s.l.]: National Aeronautics and Space Administration Scientific and Technical Information Branch, 1986.

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44

Dunham, Dana Morris. Low-speed wind-tunnel tests of single- and counter-rotation propellers. Hampton, Va: Langley Research Center, 1986.

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45

Xu, Y. L. Wind-induced fatigue loading on roof cladding of low-rise buildings. [S.l.]: Cyclone Testing Station, James Cook University of North Queensland, 1993.

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46

L, Gentry Garl, Coe Paul L, and Langley Research Center, eds. Low-speed wind-tunnel tests of single- and counter-rotation propellers. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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47

L, Gentry Carl, Dunham Dana Morris, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed wind-tunnel tests of an advanced eight-bladed propeller. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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48

L, Gentry Carl, Dunham Dana Morris, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed wind-tunnel tests of an advanced eight-bladed propeller. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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49

L, Gentry Garl, Coe Paul L, and Langley Research Center, eds. Low-speed wind-tunnel tests of single- and counter-rotation propellers. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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50

Primeau, François W. Multiple equilibria and low-frequency variability of wind-driven ocean models. Woods Hole, Mass: Massachusetts Institute of Technology, Woods Hole Oceanographic Institution, Joint Program in Oceanography/Applied Ocean Science and Engineering, 1998.

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