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1

Fish, Cheryl J. Wing span: Poems. Lewiston [N.Y.]: Mellen Poetry Press, 1992.

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2

Matthew, Accarrino, and Leahy Kate, eds. SPQR: Modern Italian food + wine. Berkeley: Ten Speed Press, 2012.

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3

Mehler, Felix Eckhart. The structural testing and modification of a full-scale ornithopter's wing spars. [Toronto]: Dept. of Aerospace Science and engineering, University of Toronto, 1997.

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4

Mehler, Felix Eckhart. The structural testing and modification of a full-scale ornithopter's wing spars. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1999.

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5

Milholen, William E. Computational analysis of semi-span model test techniques. Hampton, Virginia: National Aeronautics and Space Administration, Langley Research Center, 1996.

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6

Archibald, Russell. Span of wings: Memoirs of a working life in aircraft design encompassing a span from biplanes to Concorde-Bristol fashion. Shrewsbury: Airlife, 1992.

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7

Rinoie, Kenichi. Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing. Tokyo: National Aerospace Laboratory, 1992.

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8

Borri, Claudio, and Claudio Mannini, eds. Aeroelastic Phenomena and Pedestrian-Structure Dynamic Interaction on Non-Conventional Bridges and Footbridges. Florence: Firenze University Press, 2010. http://dx.doi.org/10.36253/978-88-6453-202-8.

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Fluid-structure and pedestrian-structure interaction phenomena are extremely important for non-conventional bridges. The results presented in this volume concern: simplified formulas for flutter assessment; innovative structural solutions to increase the aeroelastic stability of long-span bridges; numerical simulations of the flow around a benchmark rectangular cylinder; examples of designs of large structures assisted by wind-tunnel tests; analytical, computational and experimental investigation of the synchronisation mechanisms between pedestrians and footbridge structures. The present book is addressed to a wide audience including professionals, doctoral students and researchers, aiming to increase their know-how in the field of wind engineering, bluff-body aerodynamics and bridge dynamics.
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9

Millott, T. A. Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade. Moffett Field, Calif: Ames Research Center, 1994.

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10

Goodger, E. M. Transport fuels technology: From well to wheels, wings, and water. Norwich: Landfall Press, 2000.

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11

Roots and wings: The human journey from a speck of stardust to a spark of God. Toronto: Novalis, 2006.

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12

Office, National Audit. Ministry of Defence: Hercules C-130 tactical fixed wing airlift capability. London: Stationery Office, 2008.

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13

Silf, Margaret. Roots and wings: The human journey from a speck of stardust to a spark of God : the world in a grain of sand. Grand Rapids, Mich: William B. Eerdmans Pub., 2007.

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14

Tip aerodynamics from wind tunnel test of semi-span wing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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15

A Span of Wings. Society of Automotive Engineers, 1993.

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16

Cook, Laurel Olson. Wine Country Spas of California. iUniverse, Inc., 2004.

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17

Spark Notes Gone with the Wind. SparkNotes, 2002.

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18

F, Covell Peter, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Effects of winglets on a first-generation jet transport wing: VII, sideslip effects on winglet loads and selected wing loads at subsonic speeds for a full-span model. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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19

Bruce, J. M. 8 Wind-Sock Datafiles-Spad 7.C1. Example Product Brand, 1996.

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20

(Editor), T. Miyata, N. Fijisawa (Editor), and H. Yamada (Editor), eds. Long-Span Bridges and Aerodynamics. Springer-Verlag Telos, 1999.

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21

1938-, Miyata Toshio, Fujisawa N, Yamada H, and ISBAP '98 (1998 : Kōbe-shi, Japan), eds. Long-span bridges and aerodynamics. Tokyo: Springer, 1999.

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22

Sarkar, Partha P. Effect on wind turbulence on the stability on long span bridges. 1986.

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23

R, Laflin K., and United States. National Aeronautics and Space Administration., eds. Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

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24

R, Laflin K., and United States. National Aeronautics and Space Administration., eds. Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

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25

Parker, Bullock Ellen, and Langley Research Center, eds. Span reduction effects on flutter characteristics of arrow-wing supersonic transport configurations. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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26

R, Laflin K., and United States. National Aeronautics and Space Administration., eds. Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

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27

Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

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28

K, Kapania Rakesh, Barthelemy Jean-Francois M, and United States. National Aeronautics and Space Administration., eds. Sensitivity analysis of flutter response of a wing incorporating finite-span corrections. [Washington, DC: National Aeronautics and Space Administration, 1994.

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29

Evaluation, Highway Innovative Technology. Evaluation of the Con/Span Wingwall System (Cerf Report, Number to Come). American Society of Civil Engineers, 2001.

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30

Center, Ames Research, ed. An investigation of tip planform influence on the aerodynamic load characteristics of a semi-span, unswept wing and wing-tip. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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31

United States. National Aeronautics and Space Administration, ed. An investigation of tip planform influence on the aerodynamic load characteristics of a semi-span, unswept wing and wing-tip. Lawrence, Kan: University of Kansas Center for Research, Inc., 1985.

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32

Center, Langley Research, ed. Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

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33

Center, Ames Research, ed. Spanwise lift distributions and wake velocity surveys of a semi-span wing with a discontinuous twist. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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34

A Span of Wings: Memoirs of a Working Life in Aircraft Design Encompassing a Span from Biplanes to Concorde-Bristol Fashion. Society of Automotive Engineers Inc, 1993.

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35

Wind Resistant Design of Bridges in Japan. Springer, 2012.

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36

A, Reichert Bruce, and United States. National Aeronautics and Space Administration., eds. Spanwise spacing effects on the initial structure and decay of axial vortices: Under contract NAS3-27377. [Washington, DC: National Aeronautics and Space Administration, 1996.

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37

United States. National Aeronautics and Space Administration., ed. Semi-span model testing in the National Transonic Facility: Annual status report, October 1993, cooperative agreement no. NCC1, 169. [Washington, DC: National Aeronautics and Space Administration, 1993.

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38

United States. National Aeronautics and Space Administration., ed. Semi-span model testing in the National Transonic Facility: Annual status report, August 1995, cooperative agreement no. NCC1, 169. [Washington, DC: National Aeronautics and Space Administration, 1995.

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39

United States. National Aeronautics and Space Administration., ed. Semi-span model testing in the National Transonic Facility: Annual status report, August 1995, cooperative agreement no. NCC1, 169. [Washington, DC: National Aeronautics and Space Administration, 1995.

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40

Semi-span model testing in the National Transonic Facility: Annual status report, October 1993, cooperative agreement no. NCC1, 169. [Washington, DC: National Aeronautics and Space Administration, 1993.

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41

Semi-span model testing in the National Transonic Facility: Annual status report, August 1995, cooperative agreement no. NCC1, 169. [Washington, DC: National Aeronautics and Space Administration, 1995.

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42

United States. National Aeronautics and Space Administration., ed. Semi-span model testing in the National Transonic Facility: Annual status report, October 1993, cooperative agreement no. NCC1, 169. [Washington, DC: National Aeronautics and Space Administration, 1993.

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43

Silf, Margaret. Roots and Wings: The Human Journey from a Speck of Stardust to a Spark of God. Wm. B. Eerdmans Publishing Company, 2007.

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44

United States. National Aeronautics and Space Administration., ed. Semi-span model testing in the National Transonic Facility: Semi-annual status report, May 1994, cooperative agreement no. NCC1, 169. [Washington, DC: National Aeronautics and Space Administration, 1994.

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45

1944-, Carter James E., Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Analysis of transitional separation bubbles on infinite swept wings. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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46

Olson, Stuart Alve. Wind Sweeps Away the Plum Blossoms: The Principles and Techniques of Yung, Style Tai Chi Spear and Staff. Bubbling Well Pr, 1986.

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47

Cooperative agreement #NCC 2-175 entitled Investigation of a free-tip rotor configuration for research on spanwise life [i.e. lift] distributions and wake velocity surveys of a semi-span wing with a discontinuous twist: Final report. Lawrence, Kan: University of Kansas Center for Research, Inc., 1989.

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