Books on the topic 'Wing construction'

Selberg, Bruce P. Aerodynamic-structural study of canard wing, dual wing and conventional wing systems for general aviation applications. Hampton, Virginia: NASA Langley Research Center, 1985.

Fighter wing: A guided tour of an Airforce Combat wing. New York: Berkley Books, 1995.

Wood, Richard M. The natural flow wing-design concept. Hampton, Va: Langley Research Center, 1992.

Clancy, Tom. Fighter wing: A guided tour of an Air Force combat wing. New York: Berkley Books, 1995.

Clancy, Tom. Fighter wing: A guided tour of an Air Force combat wing. New York: Berkley Books, 2004.

Fighter wing: A guided tour of an Air Force combat wing. London: HarperCollins, 1995.

Valasek, John. Morphing aerospace vehicles and structures. Chichester, West Sussex: John Wiley & Sons, 2012.

American Institute of Aeronautics and Astronautics, ed. Morphing aerospace vehicles and structures. Chichester, West Sussex: John Wiley & Sons, 2012.

Wrong and dangerous: Ten right-wing myths about the constitution. Lanham, Md: Rowman & Littlefield, 2012.

Merlin, Peter W. A New twist in flight research: The F-18 active aeroelastic wing project. Washington, DC: National Aeronautics and Space Administration, Aeronautics Research Mission Directorate, 2013.

Johnsen, Frederick A. Sweeping forward: Developing & flight testing the Grumman X-29A Forward Swept Wing Research Aircraft. Washington, DC: National Aeronautics and Space Administration, Aeronautics Research Mission Directorate, 2013.

Stough, H. Paul. Flight investigation of the effect of tail configuration on stal, spin, and recovery characteristics of a low-wing general aviation research airplane. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Stough, H. Paul. Flight investigation of the effect of tail configuration on stal, spin, and recovery characteristics of a low-wing general aviation research airplane. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Keidel, Paul. The horizon: A blended wing aircraft configuration design project : NASA/USRA advanced design program, final report 1987-1988. Pomona, Calif: California State Polytechnic University Pomona, Aerospace Engineering Dept., 1988.

Ferman, M. A. A wing design method for aerospace students and home builders: Strength, weight, flutter, divergence, buckling, deflection, and twist. [Bloomington, Ind.]: Trafford Pub., 2011.

Landers, Stephen. F-16XL wing pressure distributions and shock fence results from Mach 1.4 to Mach 2.0. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

San Francisco (Calif.). Dept. of City Planning. Kaiser Permanente Medical Center, San Francisco: North wing addition and parking garage : draft environmental impact report. San Francisco, CA: The Dept., 1986.

Office, General Accounting. Military aircraft: C-17 wing flap requires additional testing : report to the Secretary of the Air Force. Washington, D.C: The Office, 1992.

Office, General Accounting. Military aircraft: C-17 wing flap requires additional testing : report to the Secretary of the Air Force. Washington, D.C: The Office, 1992.

Rudolph, Peter K. C. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

Christopher, Foster. Construction: Restructure to win. [London]: National Economic Development Office, 1991.

Kaplan, Philip. Big wings. Barnsley: Pen & Sword Aviation, 2005.

Sean, Stanwick, ed. Wine by design: The space of wine. Chichester: John Wiley, 2005.

Wolikow, Serge. La construction des territoires du Champagne (1811-1911-2011). Dijon: Éditions Universitaires de Dijon, 2012.

Wigley, D. A. Materials and techniques for model construction. Hampton, Va: Kentron International, 1985.

Loraine, Fowlow, ed. Wine by design. 2nd ed. Chichester: Wiley, 2010.

Office, General Accounting. Military aircraft: Policies on government officials' use of 89th Military Airlift Wing aircraft : report to the ranking minority member, Committee on Government Operations, House of Representatives. Washington, D.C: GAO, 1992.

Tong, Wei. Wind power generation and wind turbine design. Southampton: WIT Press, 2010.

J, Twele, ed. Wind power plants: Fundamentals, design, construction and operation. Berlin: Solarpraxis AG, 2002.

Florida, Aluminum Association of. Guide to aluminum construction in high-wind areas. Boca Raton, FL: Aluminum Association of Florida, 2001.

Gasch, R., and J. Twele. Wind power plants: Fundamentals, design, construction and operation. 2nd ed. Heidelberg: Springer, 2012.

Florida, Aluminum Association of. Guide to aluminum construction in high-wind areas. Boca Raton, FL: Aluminum Association of Florida (1650 S. Dixie Hwy., Ste. 500, Boca Raton 33432), 2002.

1944-, Stoddard Forrest S., ed. Wind turbine engineering design. New York: Van Nostrand Reinhold, 1987.

Eggleston, David M. Wind turbine engineering design. New York: Van Nostrand Reinhold, 1987.

Fernandez, Jean-Luc. La critique vinicole en France: Pouvoir de prescription et construction de la confiance. Paris: Harmattan, 2004.

Wind energy systems: Optimising design and construction for safe and reliable operation. Cambridge, UK: Woodhead Publishing, Ltd., 2011.

Rivkin, David. Wind turbine technology and design. Burlington, MA: Jones & Bartlett Learning, 2012.

Bouasse, H. Instruments a vent: Anches máetalliques et membraneuses tuyaux á anche et á bouche, orgue, instruments á embouchure de cor. Paris: Librairie Scientifique et Technique Albert Blanchard, 1986.

Victory in 'site'!: The 'who-dares-wins' of construction! Northaw, Herts: Aedificamus Press, 1987.

Hay, Jim. Response of bridges to wind. London: HMSO, 1992.

Ord-Hume, Arthur W. J. G. Autogiro: Rotary wings before the helicopter. Petersfield: Mushroom Model, 2009.

Aerodynamic-structural study of canard wing, dual wing, and conventional wing systems for general aviation applications. Rolla, Mo: University of Missouri-Rolla, 1985.

L, Cronin Donald, and United States. National Aeronautics and Space Administration., eds. Aerodynamic-structural study of canard wing, dual wing, and conventional wing systems for general aviation applications. Rolla, Mo: University of Missouri-Rolla, 1985.

United States. National Aeronautics and Space Administration., ed. Nonlinear aerodynamics and the design of wing tips. [Washington, DC: National Aeronautics and Space Administration, 1993.

Center, Ames Research, ed. A mathematical model of a tilt-wing aircraft for piloted simulation. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

United States. National Aeronautics and Space Administration., ed. Adjoint methods for aerodynamic wing design: Semi-annual progress report. [Washington, DC: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. Adjoint methods for aerodynamic wing design: Semi-annual progress report. [Washington, DC: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. The natural flow wing-design concept. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. The natural flow wing-design concept. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Boyne, Walter J., E. R. Johnson, and Drawings by Lloyd S. Jones. American Military Training Aircraft: Fixed and Rotary-Wing Trainers Since 1916. McFarland & Company, 2015.