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Ailerons -- Performance

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• Ailerons
• Airplanes -- Wings -- Performance
• Airplanes -- Performance
• Performance

• Flaps (Airplanes) -- Performance

• Performance of ailerons

• Flight investigation of an aileron and a spoiler on a wing of the X-3 airplane plan form at Mach numbers from 0.5 to 1.6 (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), by Roland D. English, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of an aileron located at two spanwise positions (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), by Robert F. Thompson, Robert T. Taylor, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), by William C. Moseley, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• NASA TN D-4141 (National Aeronautics and Space Administration ;, 1967), by Terrell W. Feistel, Robert C. Innis, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Description of an experimental (hydrogen peroxide) rocket system and its use in measuring aileron and rudder effectiveness of a light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Thomas C. O'Bryan, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Charles B. Johnson, Louis G. Kàufman, Grumman Aerospace Corporation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effect of aileron deflections on the aerodynamic characteristics of a semispan model of a subsonic energy-efficient transport (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Peter F. Jacobs and Langley Research Center (page images at HathiTrust)
• Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Wendell W. Kelley, Einar K. Enevoldson, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Hugh L. Dryden Flight Research Center, and Langley Research Center (page images at HathiTrust)
• NASA TN D-2680 (National Aeronautics and Space Administration, 1965), by Robert J. Pegg, John P. Reeder, Henry L. Kelley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, four propellers, and blowing flaps (National Aeronautics and Space Administration, 1959), by James A. Weiberg, V. Robert Page, and Ames Research Center (page images at HathiTrust)
• NASA TN D-5538 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Irving Abel, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Robert S. Swanson, E. LaVerne Priddy, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by J. D. Bird, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Paul E. Purser, Elizabeth G. McKinney, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by J. D. Bird, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Chester H. Wolowicz, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Harry E. Murray, Clarence L. Gillis, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1943), by Leo F. Fehlner, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Walter C. Williams, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), by W. C. Williams, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Robert S. Swanson, Stewart M. Crandall, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by H. A. Pearson, William S. Aiken, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Robert R. Gilruth, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick tapered, unswept wing (National Advisory Committee for Aeronautics, 1954), by Roland D. English, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Transonic flutter investigation of two 50° semispan modified-delta wings with tip ailerons (National Advisory Committee for Aeronautics, 1958), by Robert J. Platt, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Investigation of the static lateral stability and aileron characteristics of a 0.067-scale model of the Bell X-2 airplane at Mach number of 2.29, 2.78, 3.22, and 3.71 (National Advisory Committee for Aeronautics, 1958), by Roger H. Fournier, H. Norman Silvers, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• The effect of torsional flexibility on the rolling characteristics at supersonic speeds of tapered unswept wings (National Advisory Committee for Aeronautics, 1949), by Warren A. Tucker, Robert L. Nelson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65-series wings equipped with full-span slotted flaps (National Advisory Committee for Aeronautics, 1949), by Jack Fischel, James M. Watson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A Comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model having full-span flaps (National Advisory Committee for Aeronautics, 1950), by Powell M. Lovell and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Method for calculating lift distribtutions for unswept wings with flaps or ailerons by use of nonlinear section lift data (National Advisory Committee for Aeronautics, 1951), by James C. Sivells, Gertrude C. Westrick, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Wind-tunnel investigation at low speed of lateral control characteristics of an untapered 45° sweptback semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain ailerons (National Advisory Committee for Aeronautics, 1951), by Harold S. Johnson, John R. Hagerman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of aspect ratio and sweepback on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with retractable ailerons (National Advisory Committee for Aeronautics, 1951), by Jack Fischel, John R. Hagerman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of aspect ratio on the low-speed lateral control characteristics of unswept untapered low-aspect-ratio wings (National Advisory Committee for Aeronautics, 1951), by Rodger L. Naeseth, William M. O'Hare, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight tests of experimental beveled-trailing-edge Frise ailerons on a fighter airplane (National Advisory Committee for Aeronautics, 1946), by R. Fabian Goranson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1944), by Robert M. Crane, Ralph W. Holtzclaw, Ames Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series A. (National Advisory Committee for Aeronautics, 1944), by Robert M. Crane, Ralph W. Holtzclaw, Ames Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1946), by Hubert M. Drake, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1945), by J. D. Bird, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), by Francis M. Rogallo, Paul E. Purser, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), by Ira H. Abbott, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), by John G. Lowry, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), by John G. Lowry, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Wind-tunnel research comparing lateral control devices particularly at high angles of attack. III : ordinary ailerons rigged up 10 ̊when neutral (Government Printing Office, 1932), by Fred E. Weick, Carl J. Wenzinger, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Handling qualities in single-loop roll tracking tasks : theory and simulator experiments (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by T. S. Durand, Henry R. Jex, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc Systems Technology (page images at HathiTrust)
• On the theory of transonic aileron buzz (Cambridge, Massachusetts : Massachusetts Institute of Technology, Fluid Dynamics Research Laboratory, 1960., 1960), by Wiktor Eckhaus, Massachusetts Institute of Technology. Fluid Dynamics Research Laboratory, and United States. Air Force. Office of Scientific Research (page images at HathiTrust; US access only)
• Compatibility of maneuver load control and relaxed static stability (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by W. J. Rohling, W. J. Wattman, L. H. Pasley, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Company. Wichita Division (page images at HathiTrust)
• Advanced electromechanical actuation system (EMAS) development and flight test (C-141 aircraft) demonstration (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), by T. Mark Bailey, K. C. Thompson, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), Sundstrand Corporation, and Lockheed Aeronautical Systems Company. Georgia Division (page images at HathiTrust)

• Flight investigation of a V/STOL transport model with four pod-mounted lift fans (National Aeronautics and Space Administration, 1971), by William A. Newsom, Sue B. Grafton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)

• Comparison of ailerons on a rectangular and a tapered wing. (National Advisory Committee for Aeronautics, 1938), by Hartley A. Soule, William Gracey, and Langley Aeronautical Laboratory (page images at HathiTrust)

• Wind tunnel free flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Long P. Yip and Langley Research Center (page images at HathiTrust)
• Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by E. Ann Bare, Raymond C. Haddad, David E. Reubush, and Langley Research Center (page images at HathiTrust)
• Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50⁰ to 74⁰ delta wings on common fuselage (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Neal T. Frink, Thomas D. Johnson, Jarrett K. Huffman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by John W. Paulson, Daniel W. Banks, P. Frank Quinto, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A wind-tunnel investigation of the wake near the trailing edge of a deflected externally blown flap (National Aeronautics and Space Administration ;, 1974), by William G. Johnson, Gerald E. Kardas, and Langley Research Center (page images at HathiTrust)
• Pressure distributions from subsonic tests of an advanced laminar-flow-control wing with leading- and trailing-edge flaps (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Zachary T. Applin, Garl L. Gentry, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Pressure distributions on a rectangular aspect-ratio-6, slotted supercritical airfoil wing with externally blown flaps (U.S. National Aeronautics and Space Administration ;, 1976), by William G. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of Kruger nose flaps on the experimental force and moment characteristics of an oblique wing (U.S. National Aeronautics and Space Administration ;, 1976), by Edward J. Hopkins, George H. Lovette, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Flap effectiveness on subsonic longitudinal aerodynamic characteristics of a modified arrow wing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by P. Frank Quinto, John W. Paulson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Analysis of noise produced by jet impingement near the trailing edge of a flat and a curved plate (National Aeronautics and Space Administration ;, 1975), by Daniel J. McKinzie, Robert J. Burns, and Lewis Research Center (page images at HathiTrust)
• Aeroacoustic performance of an externally blown flap configuration with several flap noise suppression devices (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Daniel J. McKinzie, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flight test results of a trailing edge flap designed for direct-lift control (National Aeronautics and Space Administration ;, 1969), by Charles R. Taylor, Boeing Company, and Ames Research Center (page images at HathiTrust)
• Full-scale wind tunnel tests of a low-wing, single-engine, light plane with positive and negative propeller thrust and up and down flap deflection (National Aeronautics and Space Administration, 1971), by Edward Seckel, United States National Aeronautics and Space Administration, Langley Research Center, and Princeton University (page images at HathiTrust)
• A low speed two-dimensional study of flow separation on the GA(W)-1 airfoil with 30-percent chord Fowler flap (National Aeronautics and Space Administration, 1977), by H. C. Seetharam, W. H. Wentz, Wichita State University, and Langley Research Center (page images at HathiTrust)
• A fast-acting electrical servo for the actuation of full-span, Fowler-type wing flaps in DLC applications : a detail design study / by Frederick O. Smetana, Rafael J. Montoya, and Ronald K. Carden. (National Aeronautics and Space Administration ;, 1972), by Frederick O. Smetana, Ronald K. Carden, Rafael J. Montoya, Langley Research Center, and North Carolina State University (page images at HathiTrust)
• The Influence of wing loading on turbofan powered STOL transports with and without externally blown flaps (National Aeronautics and Space Administration ;, 1973), by R. L. Morris, Langley Research Center, and Boeing Company. Wichita Division (page images at HathiTrust)
• A method for calculating externally blown flap noise (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Martin R. Fink, United Technologies Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Calculation of the longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Michael R. Mendenhall, Selden B. Spangler, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Blade-mounted trailing edge flap control for BVI noise reduction (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by A. A. Hassan, Langley Research Center, and McDonnell Douglas Helicopter Company (page images at HathiTrust)
• The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Arthur C. Grantz, Langley Research Center, and Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept (page images at HathiTrust)
• Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory (National Aeronautics and Space Administration ;, 1975), by Boyd Perry, George C. Greene, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a powered, externally blown flap STOL transport model with two engine simulator sizes (National Aeronautics and Space Administration ;, 1975), by William G. Johnson and Langley Research Center (page images at HathiTrust)
• Simplified lifting-surface theory for flaps on wings of low and moderate aspect ratios (National Aeronautics and Space Administration ;, 1975), by Bradford H. Wick and Ames Research Center (page images at HathiTrust)
• An analytical study and wind-tunnel tests of an aeromechanical gust-alleviation system for a light airplane (National Aeronautics and Space Administration ;, 1976), by Eric C. Stewart (page images at HathiTrust)
• Thrust and wing loading requirements for short haul aircraft constrained by engine noise and field length (National Aeronautics and Space Administration ;, 1976), by Jeffrey V. Bowles, Thomas L. Galloway, Mark H. Waters, and Ames Research Center (page images at HathiTrust)
• Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles (National Aeronautics and Space Administration ;, 1975), by William C. Sleeman, William C. Hohlweg, and Langley Research Center (page images at HathiTrust)
• Wing-surface-jet interaction characteristics of an upper-surface blown model with rectangular exhaust nozzles and a radius flap (National Aeronautics and Space Administration ;, 1976), by Alvin M. Bloom, William C. Sleeman, William C. Hohlweg, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of a flare-director concept for an externally blown flap STOL aircraft (National Aeronautics and Space Administration ;, 1974), by David B. Middleton (page images at HathiTrust)
• The effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil section, comparisons with various types of flaps on other airfoil sections, and an analysis of flow and power relationships for blowing systems (National Aeronautics and Space Administration ;, 1976), by Jules B. Dods, Earl C. Watson, Ames Research Center, and United States. National Aeronautics and Space Center (page images at HathiTrust)
• Lifting-surface theory for calculating the loading induced on a wing by a flap (National Aeronautics and Space Administration ;, 1972), by Wayne Johnson, United States National Aeronautics and Space Administration, Ames Research Center, and U.S. Army Air Mobility Research and Development Laboratory (page images at HathiTrust)
• Hypersonic and transonic buzz measurements on the lower pitch flap of M2-F2 lifting entry configuration (National Aeronautics and Space Administration ;, 1972), by Robert W. Warner, Phillip R. Wilcox, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing (National Aeronautics and Space Administration ;, 1969), by Marvin P. Fink, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Simulation of decelerating landing approaches on an externally blown flap STOL transport airplane (National Aeronautics and Space Administration ;, 1974), by William D. Grantham, Perry L. Deal, Luat T. Nguyen, and Langley Research Center (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)
• Simulator evaluation of the low-speed flying qualities of an experimental STOL configuration with an externally blown flap wing or an augmentor wing (National Aeronautics and Space Administration ;, 1973), by Bruce G. Powers, David A. Kier, and Flight Research Center (U.S.) (page images at HathiTrust)
• NASA TN D-6733 (National Aeronautics and Space Administration :, 1972), by L. Keith Barker, Gene W. Sparrow, Daniel J. Crawford, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A compilation and analysis of typical approach and landing data for a simulator study of an externally blown flap STOL aircraft (National Aeronautics and Space Administration ;, 1974), by David B. Middleton, Hugh P. Bergeron, and Langley Research Center (page images at HathiTrust)
• Some effects of control profile and control trailing-edge angle on the oscillating hinge-moment and flutter characteristics of flap-type controls at transonic speeds (National Aeronautics and Space Administration, 1960), by William C. Moseley, Thomas G. Gainer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gust alleviation for a STOL transport by using elevator, spoilers, and flaps (National Aeronautics and Space Administration ;, 1974), by Frederick J. Lallman and Langley Research Center (page images at HathiTrust)
• Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators (National Aeronautics and Space Administration ;, 1974), by Danny R. Hoad and Langley Research Center (page images at HathiTrust)
• Effects of geometry and jet velocity on noise associated with an upper-surface-blowing model (National Aeronautics and Space Administration ;, 1977), by Lorenzo R. Clark, James C. Yu, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by I. Elizabeth Garner, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Robert B. Liddell, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Marvin Pitkin, Robert O. Schade, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Jack Fischel, John M. Riebe, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by M. Leroy Spearman, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by Thomas A. Toll, Margaret F. Ivey, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1945), by John M. Riebe, Elizabeth G. McKinney, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45° sweptback wing of aspect ratio 4 (National Advisory Committee for Aeronautics, 1957), by Kenneth P. Spreemann, William J. Alford, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Comparison of semispan data obtained in the Langley two-dimensional low-turbulence pressure tunnel and full-span data obtained in the Langley 19-foot pressure tunnel for a wing with a 40⁰ sweepback of the 0.27-chord line (National Advisory Committee for Aeronautics, 1949), by Jones F. Cahill, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Load distributions associated with controls at supersonic speeds (National Advisory Committee for Aeronautics, 1953), by K. R. Czarnecki, Douglas R. Lord, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Effects of twist and camber on the low-speed longitudinal stability characteristics of a 45° swept-back wing of aspect ratio 8 at Reynolds numbers from 1.5 x 10⁶ to 4.8 x 10 as determined by pressure distributions, force tests, and calculations (National Advisory Committee for Aeronautics, 1952), by George L. Pratt, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35°, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1950), by Robert F. Thompson, United States. National Adviosry Committee for Aeronautics, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps (National Advisory Committee for Aeronautics, 1948), by James C. Sivells, Stanley H. Spooner, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Low-speed experimental investigation of a thin, faired, double-wedge airfoil section with nose and trailing-edge flaps (National Advisory Committee for Aeronautics, 1949), by Leonard M. Rose, John M. Altman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results (National Advisory Committee for Aeronautics, 1950), by John D. Bird, Byron M. Jaquet, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds (National Advisory Committee for Aeronautics, 1951), by John DeYoung and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Method for calculating lift distribtutions for unswept wings with flaps or ailerons by use of nonlinear section lift data (National Advisory Committee for Aeronautics, 1951), by James C. Sivells, Gertrude C. Westrick, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Some theoretical characteristics of trapezoidal wings in supersonic flow and a comparison of several wing-flap combinations (National Advisory Committee for Aeronautics, 1951), by Robert O. Piland and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of wing thickness and sweep on the oscillating hinge-moment and flutter characteristics of a flap-type control at transonic speeds (National Aeronautics and Space Administration, 1959), by William C. Moseley, Thomas G. Gainer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Recent information on flap and tip controls (National Advisory Committee for Aeronautics, 1953), by Douglas R. Lord, K. R. Czarnecki, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Recent control studies (National Advisory Committee for Aeronautics, 1959), by John G. Lowry and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4 (National Advisory Committee for Aeronautics, 1957), by Earl D. Knechtel, George Lee, Ames Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps (National Advisory Committee for Aeronautics, 1948), by Jack D. Brewer, Josephine F. Polhamus, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1943), by H. Page Hoggard, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), by Isidore G. Recant, Arthur R. Wallace, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), by Ira H. Abbott, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), by Ira H. Abbott, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), by John G. Lowry, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1941), by John G. Lowry, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), by John G. Lowry, Thomas A. Toll, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), by Lawrence D. Guy, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Aircraft accident report : inadvertent in-flight slat deployment, China Eastern Airlines flight 583, McDonnell Douglas MD-11, B-2171, 950 nautical miles south of Shemya, Alaska, April 6, 1993. (National Transportation Safety Board ;, 1993), by United States. National Transportation Safety Board (page images at HathiTrust)
• Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings (1940), by Abe Silverstein, S. Katzoff, and Langley Aeronautical Laboratory (page images at HathiTrust)
• An investigation of separated flows on two-dimensional models at Mach numbers 5 and 8 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), by A. L. Baer, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Supersonic near free molecule flow over a specularly reflecting flat plate with a deflected flap (Los Angeles, California : Space Systems and Ballistic Systems Divisions, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1966., 1966), by Charles R. Ortloff, United States. Air Force. Systems Command. Space Systems Division, and Aerospace Corporation (page images at HathiTrust)
• Low-speed investigations of 'Apex Fence' and 'Cavity Flap' concepts on a 60 degree delta configuration (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1987., 1987), by Dhanvada M. Rao, Charles T. L. Mills, Keith D. Hoffler, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Vigyan Research Associates (page images at HathiTrust)
• NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1944), by Felicien F. Fullmer, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• STOL tactical aircraft investigation - externally blown flap. Volume I, Configuration definition. Supplement I, Aerodynamic trades of flap and roll control system (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)
• 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)
• STOL tactical aircraft investigation - externally blown flap. Volume V, Flight control technology. Part I, Control system mechanization trade studies (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), by Robert W. Phillips, Air Force Flight Dynamics Laboratory (U.S.), Rockwell International. Los Angeles Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)

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