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Takeoff

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• Airplanes -- Takeoff
• Airplanes, Military -- Takeoff
• Seaplanes -- Takeoff
• Supersonic transport planes -- Takeoff
• Transport planes -- Takeoff

• Technology requirements for advanced earth orbital transportation systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by A. K. Hepler, E. L. Bangsund, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Take-off distances of a supersonic transport configuration as affected by airplane rotation during the take-off run (National Aeronautics and Space Administration, 1961), by Albert W. Hall, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Consideration of some aerodynamic characteristics during take-off and landing of jet airplanes (National Aeronautics and Space Administration, 1959), by John M. Riebe and Langley Research Center (page images at HathiTrust)

• Safety through steep gradient aircraft : a survey of the status and effects of vertical and near-vertical take-off and landing (Daniel and Florence Guggenheim Aviation Safety Center, 1955), by Cornell University. Daniel and Florence Guggenheim Aviation Safety Center (page images at HathiTrust)
• The finite aspect ratio jet flap. (Cornell Aeronautical Laboratory, 1959), by Richard A. Hartunian (page images at HathiTrust)
• A flight test comparison of take-off performance of two liaison type airplane configurations. (Cornell Aeronautical Laboratory, Inc., 1959), by Donald W. Rhoads (page images at HathiTrust)
• Field hearing to receive testimony on the crash of USAir flight 405 : hearing before a subcommittee of the Committee on Appropriations, United States Senate, One Hundred Second Congress, second session. (U.S. G.P.O. :, 1992), by United States. Congress. Senate. Committee on Appropriations (page images at HathiTrust)
• A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Raymond L. Barger, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Validation of a flexible aircraft take-off and landing analysis (FATOLA) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Huey D. Carden, John R. McGehee, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Flight evaluation of stabilization and command augmentation system concepts and cockpit displays during approach and landing of a powered-lift STOL aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by James A. Franklin, Gordon H. Hardy, Robert C. Innis, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Vertical and lateral stiffness characteristics of aircraft tires (National Aeronautics and Space Administration ;, 1969), by G. H. Nybakken, Samuel K. Clark, Langley Research Center, and Ohio State University (page images at HathiTrust)
• Influence of high-turbine-inlet-temperature engines in a methane-fueled SST when takeoff jet noise limits are considered (National Aeronautics and Space Administration, 1968), by Robert W. Koenig, Gerald A. Kraft, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical study of takeoff and landing performance for a jet STOL transport configuration with full-span, externally blown, triple-slotted flaps (National Aeronautics and Space Administration ;, 1973), by Harold P. Washington, John T. Gibbons, and Flight Research Center (U.S.) (page images at HathiTrust)
• Technique for calculating optimum takeoff and climbout trajectories for noise abatement (National Aeronautics and Space Administration :, 1969), by Heinz Erzberger, Homer Q. Lee, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Takeoff certification considerations for large subsonic and supersonic transport airplanes using the Ames Flight Simulator for Advanced Aircraft (National Aeronautics and Space Administration ;, 1973), by C. Thomas Snyder, United States Federal Aviation Administration, and Ames Research Center (page images at HathiTrust)
• Ground noise measurements during landing, take-off, and flyby operations of a four-engine turbopropeller STOL airplane (National Aeronautics and Space Administration ;, 1971), by David A. Hilton, Domenic J. Maglieri, Herbert R. Henderson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Versuche an Doppeldeckern zur Bestimmung ihrer Eigengeschwindigkeit und Flugwinkel (Verlag von Julius Springer, 1913), by Wilhelm Hoff (page images at HathiTrust; US access only)
• Brake performance of the McDonnell Douglas DC-10-30/40 during high speed, high energy rejected takeoffs (The Board ;, 1990), by United States. National Transportation Safety Board (page images at HathiTrust)
• Aircraft wake vortex takeoff tests at O'Hare International Airport (Office of Research and Development Service, U.S. Department of Transportation, Federal Aviation Administration ;, 1994), by Joseph Yarmus, John A. Volpe National Transportation Systems Center (U.S.), and United States. Federal Aviation Administration. Office of Research and Development Service (page images at HathiTrust)
• Runway overruns following high speed rejected takeoffs. (National Transportation Safety Board ;, 1990), by United States. National Transportation Safety Board (page images at HathiTrust)
• Analysis of the effects of boundary-layer control on the take-off performance characteristics of a liaison-type airplane (National Advisory Committee for Aeronautics, 1948), by Elmer A. Horton, John H. Quinn, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of a 90° cross wind on the take-off distance of a light airplane equipped with a cross-wind landing gear (National Advisory Committee for Aeronautics, 1949), by Seth B. Anderson, William H. McAvoy, Burnett L. Gadeberg, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Supersonic transport airport and community jet noise during takeoff and initial climb (National Aeronautics and Space Administration ;, 1967), by John B. Whitlow, Gerald A. Kraft, Robert W. Koenig, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aircraft operations on unsurfaced soil, soil measurements and analyses, Project Rough Road Alpha. (Army Engineer Waterways Experiment Station, 1963), by Waterways Experiment Station (U.S.) (page images at HathiTrust)
• Civil Aeronautics Board planning study : STOL/VTOL air transportation systems (U.S. Civil Aeronautics Board, 1970), by Carl Hintze and United States. Civil Aeronautics Board. Bureau of Economics (page images at HathiTrust)
• Special study : U.S. General Aviation takeoff accidents : the role of preflight preparation. (NTSB :, 1976), by United States. National Transportation Safety Board (page images at HathiTrust)
• The Behavior of conventional airplanes in situations thought to lead to most crashes (National Advisory Committee for Aeronautics ;, 1931), by Fred E. Weick and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Airport runway and taxiway design (Airborne Instruments Laboratory, 1960), by M. A. Warskow, Porter & O'Brien, and Airborne Instruments Laboratory (page images at HathiTrust; US access only)
• Aircraft accident report : Horizon Air, Inc. Dehavilland DHC-8, Seattle-Tacoma International Airport, Seattle, Washington, April 15, 1988 (National Transportation Safety Board, 1989), by United States. National Transportation Safety Board (page images at HathiTrust)
• Aircraft accident report : Ryan International Airlines DC-9-15, N565PC loss of control on take off, Cleveland-Hopkins International Airport Cleveland, Ohio February 17, 1991. (National Transportation Safety Board ;, 1991), by United States. National Transportation Safety Board (page images at HathiTrust)
• Study of the effect of departure procedures on the noise produced by jet transport aircraft : technical report (FAA, 1965), by William J. Galloway, Karl S. Pearsons, A. C. Pietrasanta, United States. Federal Aviation Agency, and Beranek Bolt (page images at HathiTrust)
• An analysis of ground-flight loads measured on the instrumented B-727 N40 (Federal Aviation Administration, Office of Aviation Research ;, 1995), by William M. Cavage, Terence Barnes, Tom DeFiore, Federal Aviation Administration Technical Center (U.S.), Galaxy Scientific Corporation, and United States. Office of Aviation Research (page images at HathiTrust)
• Analysis of aircraft noise levels in the vicinity of start-of-takeoff roll at Baltimore-Washington International Airport (U.S. Federal Aviation Administration ;, 1992), by Richard D. Horonjeff, John A. Volpe National Transportation Systems Center (U.S.), Miller Harris, and United States Federal Aviation Administration (page images at HathiTrust)
• Research requirements for future visual guidance systems (FAA Technical Center ;, 1994), by Harold W. Olson, Thomas H. Paprocki, MITECH Inc, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Soft ground arresting system for airports (Federal Aviation Administration Technical Center ;, 1993), by James C. White, Satish Kumar Agrawal, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• National airspace system : flight planning operational concept (NAS-SR-1310) (Federal Aviation Administration, Advanced System Design Service ;, 1989), by Alexandra Argyropoulos, Mitre Corporation, and United States. Federal Aviation Administration. Advanced System Design Service (page images at HathiTrust)
• National airspace system : airspace management operational concept (NAS-SR-1321) (Federal Aviation Administration, Advanced System Design Service ;, 1989), by Stephanie B. Fraser, Mitre Corporation, and United States. Federal Aviation Administration. Advanced System Design Service (page images at HathiTrust)
• National airspace system approach and departure sequencing operational concept (NAS-SR-1322) (Federal Aviation Administration, Advanced System Design Service ;, 1989), by Joseph P. Iadeluca, Mitre Corporation, and United States. Federal Aviation Administration. Advanced System Design Service (page images at HathiTrust)
• National airspace system : airport movement area control operational concept, NAS-SR-13211 (Federal Aviation Administration, Advanced System Design Service ;, 1989), by A. Lucille Springen, Mitre Corporation, and United States. Federal Aviation Administration. Advanced System Design Service (page images at HathiTrust)
• Trainer attachment, visual simulator SMK 22/F37A-T (Wright-Patterson Air Force Base, Ohio : Training Equipment Division, Directorate of Crew Subsystems Engineering, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Fairchild Stratos Corporation and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• STOL tactical aircraft investigation - externally blown flap. Volume III, Performance methods and takeoff and landing rules (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Dirk J. Renselaer, Air Force Flight Dynamics Laboratory (U.S.), Rockwell International. Los Angeles Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)

• Pilot study of response of CV-2 aircraft to irregular terrain (Waterways Experiment Station, 1967), by A. J. Green and Edgar S. Rush (page images at HathiTrust)

• Effect of afterbody length and keel angle on minimum depth of step for landing stability and on take-off stability of a flying boat (National Advisory Committee for Aeronautics, 1948), by Roland E. Olson, Norman S. Land, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• An investigation of the hydrodynamic characteristics of a dynamic model of a transonic seaplane design having a planing-tail hull (Washington, D.C. : National Advisory Committee for Aeronautics, [1956], 1956), by Archibald E. Morse, Ulysse J. Blanchard, David R. Woodward, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by William D. Grantham, Perry L. Deal, Paul M. Smith, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• NASA TN D-4396 (National Aeronautics and Space Administration ;, 1968), by C. Thomas Snyder, Charles T. Jackson, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Terminal-area flight procedures and route design for supersonic transport New York-transatlantic operations (National Aeronautics and Space Administration ;, 1972), by Richard H. Sawyer, Milton D. McLaughlin, and Langley Research Center (page images at HathiTrust)

• Simulator study of flight characteristics of several large dissimilar, cargo transport airplanes during approach and landing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by William D. Grantham and Langley Research Center (page images at HathiTrust)
• Simulator study of flight characteristics of a large twin-fuselage cargo transport airplane during approach and landing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by William D. Grantham and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• NASA TN D-5862 (National Aeronautics and Space Administration :, 1970), by William D. Grantham, Robert W. Sommer, Perry L. Deal, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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