Libros sobre el tema "Aircraft Wing"

Keane, Andrew J., András Sóbester y James P. Scanlan. Small Unmanned Fixed-wing Aircraft Design. Chichester, UK: John Wiley & Sons, Ltd, 2017. http://dx.doi.org/10.1002/9781119406303.

Bolonkin, Alexander. Estimated benefits of variable-geometry wing camber control for transport aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Drain, Richard. 5th Bomb Wing: History of aircraft assigned. [S.l.]: R.E. Drain, 1991.

Pantham, Satyaraj. Classical dynamics of variable sweep wing aircraft. Bangalore, India: Dept. of Aerospace Engineering, Indian Institute of Science, 1993.

Phillips, James D. Modal control of an oblique wing aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Kroo, Ilan. The aerodynamic design of oblique wing aircraft. New York: American Institute of Aeronautics and Astronautics, 1986.

Jan, Koniarek, ed. Poland's PZL gull-wing fighters: Part One: P.1 through P.8. St. Paul, Minnesota: Phalanx Publishing Company, 1995.

Smith, Peter J. Damage tolerant composite wing panels for transport aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Copyright Paperback Collection (Library of Congress), ed. Punk's wing. New York: Signet, 2003.

Martin, John. On a wing and a microwave. [S.l.]: [s.n.], 1988.

Myhra, David. The Horten brothers and their all-wing aircraft. Atglen, PA: Schiffer Pub., 1998.

Ko, William L. Buckling characteristics of hypersonic aircraft wing tubular panels. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1989.

Sturtivant, Ray. Fleet air arm fixed-wing aircraft since 1946. Tonbridge: Air Britain (Historians) Ltd., 2004.

Sweeney, Joseph Woods III. Computer aided deflection measurements of an aircraft wing. Monterey, Calif: Naval Postgraduate School, 1987.

Hirschel, Ernst Heinrich, Arthur Rizzi, Christian Breitsamter y Werner Staudacher. Separated and Vortical Flow in Aircraft Wing Aerodynamics. Berlin, Heidelberg: Springer Berlin Heidelberg, 2021. http://dx.doi.org/10.1007/978-3-662-61328-3.

Cook, M. V. The aerodynamic design optimisation of a forward swept wing fighter aircraft. Cranfield, U.K: College of Aeronautics, Cranfield Institute of Technology, 1987.

Keogan, Joseph. The Igor I. Sikorsky aircraft legacy: The chronology of fixed-wing and rotary-wing aircraft of Igor I. Sikorsky and the Sikorsky Aircraft Company. Stratford, CT: Igor I. Sikorsky Historical Archives, Inc., 2003.

C, Patterson James. Evaluation of installed performance of a wing-tip-mounted pusher turboprop of a semispan wing. Hampton, Va: Langley Research Center, 1987.

Vincent, James H. Application of modern control design methodology to oblique wing research aircraft. Palo Alto, Calif: Systems Control Technology, Inc., 1991.

Pendergraft, Odis C. Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model. Hampton, Va: Langley Research Center, 1992.

Attack helicopters: A history of rotary-wing combat aircraft. London: Greenhill, 1987.

Kozek, Martin y Alexander Schirrer, eds. Modeling and Control for a Blended Wing Body Aircraft. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-10792-9.

Attack helicopters: A history of rotary-wing combat aircraft. Baltimore, MD: Nautical & Aviation Pub. Co. of America, 1987.

Turk, Thomas Andrew. Aircraft wing anti-icing system: Modelling, integration, and validation. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.

Phelps, Arthur E. Description of the U.S. Army small-scale 2-meter rotor test system. Hampton, Va: Langley Research Center, 1987.

Ferguson, Samuel W. Rotorwash computer model - user's guide. Washington, D. C: Federal Aviation Administration, 1991.

Only the wing: Reimar Horten's epic quest to stabilize and control the all-wing aircraft. Washington, D.C: Smithsonian Institution Scholarly Press, 2011.

Carlson, John R. Integration effects of pylon geometry on a high-wing transport airplane. Hampton, Va: Langley Research Center, 1989.

Martin, Colin A. Surface pressure measurements on the wing of a wind tunnel model during steady rotation. Melbourne, Australia: Aeronautical Research Laboratory, 1991.

Siegers, F. Design synthesis for swept-wing combat aircraft incorporating stealth technology. Cranfield, Bedford, England: Dept. of Aerospace Technology, College of Aeronautics, Cranfield University, 1994.

Rider, James. Sliding mode control of fixed and rotary-wing vstol aircraft. London: University of East London, 1999.

Seddon, Philip J. Tracking wildlife radio-tag signals by light fixed-wing aircraft. Wellington, N.Z: Dept. of Conservation, 2004.

Keith, Dexter, ed. MiG-23/27 Flogger: Soviet swing-wing fighter/strike aircraft. Hinckley: Aerofax, 2005.

Curry, Robert E. Dynamic ground effect for a cranked arrow wing airplane. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Wrenn, Gregory A. Multilevel decomposition approach to the preliminary sizing of a transport aircraft wing. Hampton, Va: Langley Research Center, 1990.

Coffee on the wing beam. Clear Lake, Wash: Knights of the Red Branch Press, 1997.

Saltzman, Edwin J. In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft). Edwards, Calif: Dryden Flight Research Facility, 1994.

Murri, Daniel G. Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing. Hampton, Va: Langley Research Center, 1987.

Skarsgard, Andrew Jonathan. The implementation of flapping-wing propulsion for a full-scale ornithopter. [Downsview, Ont.]: Department of Aerospace Science and Engineering, University of Toronto, 1991.

C, Wilson John. Wind tunnel test results of a 1/8-scale fan-in-wing model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamics of rotorcraft. Neuilly sur Seine, France: AGARD, 1990.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamics of rotorcraft. Neuilly-sur-Seine: AGARD, 1990.

Wright Field Library. Reference Branch., ed. Rotary wing aircraft: Bibliography. Wright Field, Ohio: Army Air Force Materiel Command for the Engineering Divison, 1988.

L, Sager Garrett y United States. National Aeronautics and Space Administration., eds. Aircraft wing structure detail design. [Washington, DC: National Aeronautics and Space Administration, 1993.

H, Chen H. y United States. National Aeronautics and Space Administration., eds. Aeroelastic analysis of aircraft: Wing and wing/fuselage configurations. [Washington, DC: National Aeronautics and Space Administration, 1997.

Westland Fixed Wing Aircraft 1915-1953. Fonthill Media, 2018.

Ring wing aircraft. Styro-flyer twin. [Washington, D.C.?]: NASA Aerospace Education Services Project, 1991.

S, Alag Gurbux, Gilyard Glenn B y Dryden Flight Research Facility, eds. Aeroelastic control of oblique-wing aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

Third Marine Aircraft Wing (Operation Iraqi Freedom). Marine Corps Association, 2004.

United States. National Aeronautics and Space Administration., ed. Aeroelasticity of wing and wing-body configurations on parallel computers. San Jose, CA: MCAT Institute, 1995.