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Stalling (Aerodynamics)

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Aerofoils -- Stalling
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Stall (fluid dynamics)

Filed under: Stalling (Aerodynamics)

Basic studies of rotating stall and an investigation of flow-instability sensing devices (Air Force Aero-propulsion Laboratory, Research and Technology Division, Air Force Systems Command, 1965), by Cornell Aeronautical Laboratory, Gary R. Ludwig, and William Gordon Brady (page images at HathiTrust)
Preliminary study of three-dimensional rotating stall (Wright Air Development Center, Air Research and Development Command, United States Air Force, Wright-Patterson Air Force Base, 1959), by F. K. Moore, Armed Services Technical Information Agency (U.S.), and Wright Air Development Center (page images at HathiTrust)
Wind tunnel tests of thin airfoils oscillating near stall. (U.S. Army Aviation Materiel Laboratories, 1969), by Franklyn J. Davenport, Jaan Liiva, Lewis Gray, and U.S. Army Aviation Materiel Laboratories (page images at HathiTrust)
Two-dimensional tests of airfoils oscillating near stall. (U.S. Army Aviation Materiel Laboratories, 1968), by Lewis Gray, Jaan Liiva, and U.S. Army Aviation Materiel Laboratories (page images at HathiTrust)
Propeller blade stall flutter investigation. Contract no. AF 33(616)-2670. (Cornell Aeronautical Laboratory, Inc., 1958), by William Gordon Brady (page images at HathiTrust)
Investigation of lateral stability at stall. (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1954), by Gifford Bull (page images at HathiTrust)
Critical regimes of supersonic jet aircraft; stall and spin (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1969), by Mikhail Grigorʹevich Kotik (page images at HathiTrust; US access only)
Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by H. Paul Stough, James M. Patton, Daniel J. DiCarlo, and Langley Research Center (page images at HathiTrust)
Flight characteristics of a modified Schweizer SGS 1-36 sailplane at low and very high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Alex G. Sim and Dryden Flight Research Facility (page images at HathiTrust)
Airfoil interaction with an impinging vortex (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Kenneth W. McAlister, C. Tung, United States. Army Aviation Systems Command, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Water-tunnel experiments on an oscillating airfoil at RE = 21,000 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Kenneth W. McAlister, Lawrence W. Carr, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Flight investigation of stall, spin, and recovery characteristics of a low-wing, single-engine, T-tail light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by H. Paul Stough, James M. Patton, Daniel J. DiCarlo, and Langley Research Center (page images at HathiTrust)
Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by H. Paul Stough, Steven M. Sliwa, James M. Patton, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Wind-tunnel investigation of the tail-spoiler concept for stall prevention on general aviation airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Dale R. Satran, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Dynamic stall experiments on the NACA 0012 airfoil (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Kenneth W. McAlister, William J. McCroskey, Lawrence W. Carr, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A laser velocimeter flow survey above a stalled wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Warren H. Young, Danny R. Hoad, James F. Meyers, Langley Research Center, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Simulator study of the stall departure characteristics of a light general aviation airplane with and without a wing-leading-edge modification (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Donald R. Riley and Langley Research Center (page images at HathiTrust)
Effects of wing-leading-edge modifications on a full-scale, low-wing general aviation airplane : wind-tunnel investigation of high-angle-of-attack aerodynamic characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by William A. Newsom, Dale R. Satran, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Joseph L. Johnson (page images at HathiTrust)
Analytical investigation of the effects of blade flexibility, unsteady aerodynamics, and variable inflow on helicopter rotor stall characteristics (National Aeronautics and Space Administration, 1971), by E. D. Bellnger, United States National Aeronautics and Space Administration, United Aircraft Corporation. Research Laboratories, and Langley Research Center (page images at HathiTrust)
Experimental studies of flow separation and stalling on a two-dimensional airfoil at low speeds (National Aeronautics and Space Administration, 1975), by H. C. Seetharam, W. H. Wentz, Wichita State University, and Langley Research Center (page images at HathiTrust)
Analysis of oscillatory pressure data including dynamic stall effects (National Aeronautics and Space Administration ;, 1974), by F. O. Carta, Langley Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
Comparison of dynamic stall phenomena for pitching and vertical translation motions (National Aeronautics and Space Administration ;, 1977), by T. Fukushima, L. U. Dadone, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A theory of rotating stall of multistage axial compressors (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by F. K. Moore, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Sibley School of Mechanics and Aerospace Engineering, and Lewis Research Center (page images at HathiTrust)
Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by E. Richard White, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Kentron International, and Langley Research Center (page images at HathiTrust)
Rotary balance data for a single-engine trainer design for an angle-of-attack range of 8 ̊to 90/̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Paul Pantason, Waldo Dickens, Langley Research Center, Inc Bihrle Applied Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Stall propagation in a cascade of airfoils (U.S. G.P.O., 1960), by Anthony R. Kriebel, Richard G. Schwind, Barry S. Seidel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Full-scale wind-tunnel test of the VZ-2 VTOL Airplane with particular reference to the wing stall phenomena (National Aeronautics and Space Administration, 1963), by Robert G. Mitchell and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-2462 (National Aeronautics and Space Administration :, 1964), by George E. Sweet, Matthew M. Winston, Julian L. Jenkins, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
Comparison of three methods for calculation of helicopter rotor blade loading and stresses due to stall (National Aeronautics and Space Administration ;, 1974), by Wayne Johnson, U.S. Army Air Mobility Research and Development Laboratory, and Ames Research Center (page images at HathiTrust)
A piloted simulation study of operational aspects of the stall pitch-up (National Aeronautics and Space Administration ;, 1967), by Maurice D. White, George E. Cooper, and Ames Research Center (page images at HathiTrust)
Laser velocimeter systems analysis applied to a flow survey above a stalled wing (National Aeronautics and Space Administration ;, 1977), by Warren H. Young, Timothy E. Hepner, James F. Meyers, Langley Directorate, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Stalled and stall-free performance of axial-flow compressor stage with three inlet-guide-vane and stator-blade settings (National Aeronautics and Space Administration ;, 1977), by Donald C. Urasek, Walter S. Cunnan, Ronald J. Steinke, and Lewis Research Center (page images at HathiTrust)
Wind-tunnel tests of a full-scale model of a light twin-engine airplane with fixed auxiliary airfoil or leading-edge slot (National Aeronautics and Space Administration ;, 1974), by Marvin P. Fink, Lucy C. White, James P. Shivers, and Langley Research Center (page images at HathiTrust)
NASA TN D-3370 (National Aeronautics and Space Administration :, 1966), by Bruce G. Powers, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-5826 (National Aeronautics and Space Administration :, 1970), by Richard A. Martin, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Effect of Reynolds number and engine nacelles on the stalling characteristics of a model of a twin-engine light airplane (National Aeronautics and Space Administration ;, 1972), by Vernard E. Lockwood and Langley Research Center (page images at HathiTrust)
Analysis of the development of dynamic stall based on oscillating airfoil experiments (National Aeronautics and Space Administration ;, 1977), by Lawrence W. Carr, William J. McCroskey, Kenneth W. McAlister, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Preliminary study of some factors which affect the stall-flutter characteristics of thin wings (National Advisory Committee for Aeronautics, 1952), by A. Gerald Rainey, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Spinning and related problems at high angles of attack for high-speed airplanes (National Advisory Committee for Aeronautics, 1956), by Walter J. Klinar, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Preliminary results for a free-flight investigation at transonic and supersonic speeds of longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3 (National Advisory Committee for Aeronautics, 1950), by Clarence L. Gillis, A. James Vitale, Robert F. Peck, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Stalling of helicopter blades (National Advisory Committee for Aeronautics, 1946), by F. B. Gustafson, G. C. Myers, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
General aviation pilot stall awareness training study (Dept. of Transportation, Federal Aviation Administration, Systems Research & Development Service ;, 1976), by William C. Hoffman, Walter M. Hollister, Aerospace Systems Inc, and United States. Federal Aviation Administration. Systems Research and Development Service (page images at HathiTrust)
A study of lightplane stall avoidance and suppression (Dept. of Transportation, Federal Aviation Administration, System Research & Development Service ;, 1977), by David R. Ellis, Princeton University. Flight Research Laboratory, and United States. Federal Aviation Administration. Systems Research and Development Service (page images at HathiTrust)
An investigation of the learning of stall perception (Washington, D.C. : Civil Aeronautics Administration, Division of Research, [1948?], 1948), by Floyd Carlton Dockeray and David Bakan (page images at HathiTrust)
Aircraft accident report : takeoff stall in icing conditions, USAir Flight 405, Fokker F-28, N485US, LaGuardia Airport, Flushing, New York, March 22, 1992 (National Transportation Safety Board, 1993), by United States. National Transportation Safety Board (page images at HathiTrust)
Stall/spin/flight simulation (Federal Aviation Administration Technical Center ;, 1989), by M. G. Nagati, Wichita State University. Institute for Aviation Research, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
Lift hysteresis at stall as an unsteady boundary-layer phenomenon (U.S. Government Printing Office, 1956), by F. K. Moore and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Research on rotating stall in axial flow compressors. Part II, On the separation of the unsteady laminar boundary layer (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by R. A. Hartunian, F. K. Moore, Wright Air Development Center, United States. Air Force. Air Research and Development Command, and Armed Services Technical Information Agency (U.S.) (page images at HathiTrust)
Investigation of flying qualities of military aircraft at high angles of attack. Volume I, Technical results (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Donald E. Johnston, Jeffrey R. Hogge, Irving L. Ashkenas, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
Investigation of flying qualities of military aircraft at high angles of attack. Volume II, Appendices (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Donald E. Johnston, Gary L. Teper, Jeffrey R. Hogge, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
Theoretical and experimental investigation of flow over single and double backward facing steps ([Washington, D.C.] : [United States Air Force, Office of Scientific Research], [1961], 1961), by Douglas Eugene Abbott, S. J. Kline, United States. Air Force. Office of Scientific Research, and Stanford University. Department of Mechanical Engineering (page images at HathiTrust)
Post stall maneuvers and thrust vectoring performance analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), by L. Earl Miller, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Theoretical investigation of processes to dynamic stall and control (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, United States Air Force, 1997., 1997), by J. D. A. Walker, United States. Air Force. Office of Scientific Research, and Lehigh University. Department of Mechanical Engineering and Mechanics (page images at HathiTrust)
Development of LES methodology for the analysis of high-Reynolds number 2-D and 3-D dynamic stall phenomenon (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Aerospace Sciences, 1997., 1997), by K. N. Ghia, Urmila Ghia, University of Cincinnati. Department of Aerospace Engineering and Engineering Mechanics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Operational utility survey: supermaneuverability (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), by William L. Hamilton, Andrew M. Skow, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Eidetics Incorporated (page images at HathiTrust)
Investigation of helicopter control loads induced by stall flutter (Fort Eustis, Virginia : U.S. Army Aviation Materiel Laboratories, 1970., 1970), by P. J. Arcidiacono, H. L. Elman, L. M. Casellini, F. O. Carta, U.S. Army Aviation Materiel Laboratories, and United Aircraft Corporation. Sikorsky Aircraft Division (page images at HathiTrust)

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