Spin (Aerodynamics) -- Computer programsSee also what's at your library, or elsewhere.
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Filed under: Spin (Aerodynamics) Spin recovery training hearings before the Subcommittee on Investigations and Oversight of the Committee on Science and Technology, U.S. House of Representatives, Ninety-sixth Congress, second session, June 17, 18, 19, 1980. (U.S. G.P.O., 1981), by United States. Congress. House. Committee on Science and Technology. Subcommittee on Investigations and Oversight (page images at HathiTrust) Spin recovery training report (U.S. G.P.O., 1980), by United States. Congress. House. Committee on Science and Technology. Subcommittee on Investigations and Oversight (page images at HathiTrust) Bausteine zur Flugbahn- und Kreisel-Theorie (Verlag von R. Eisenschmidt, 1914), by August Dähne (page images at HathiTrust; US access only) 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) Measurements of pressure on the tail and aft fuselage of an airplabne model during rotary motions at spin attitudes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by James S. Bowman, Colin A. Martin, Randy S. Hultberg, and Langley Research Center (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) A spin-recovery parachute system for light general-aviation airplanes (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Charles F. Bradshaw, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust) Spin-tunnel investigation of a 1/13-scale model of the NASA AD-1 oblique-wing research aircraft (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by William L. White, James S. Bowman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust) Analytical investigation of the spin and recovery characteristics of a supersonic trainer airplane having a 24° swept wing (National Aeronautics and Space Administration, 1962), by William D. Grantham and United States National Aeronautics and Space Administration (page images at HathiTrust) Semiempirical method for prediction of aerodynamic forces and moments on a steadily spinning light airplane (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), by Bandu N. Pamadi, Lawrence W. Taylor, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust) Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 (National Aeronautics and Space Administration ;, 1977), by Earl R. Keener and United States National Aeronautics and Space Administration (page images at HathiTrust) Pseudosteady-state analysis of nonlinear aircraft maneuvers (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by John W. Young, Katherine G. Johnson, Albert A. Schy, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust) Determination of corrections to flow direction sensor measurements over an angle-of-attack range from 0 ̊to 85 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Thomas M. Moul 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) Spinning filamentary disk (National Aeronautics and Space Administration, 1964), by A. C. Kyser, Astro Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust) F-15 rotary balance data for an angle-of-attack range of 8⁰ to 90⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Billy Barnhart, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley 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 agricultural airplane configuration for an angle-of-attack range of 8t̊o 90/̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by William Mulcay, Julio Chu, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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) Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 ̊to 90 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by William Mulcay, Robert A. Rose, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust) Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊ II, High-wing model A (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by William Mulcay, Robert A. Rose, Langley Research Center, and Inc Bihrle Applied Research (page images at HathiTrust) Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 35.̊ III, Effect of wing leading-edge modifications model A (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by William Bihrle, William Mulcay, Langley Research Center, and Inc Bihrle Applied Research (page images at HathiTrust) NASA TR R-57 (National Aeronautics and Space Administration ;, 1960), by A. I. Neihouse, Stanley H. Scher, Walter J. Klinar, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-6091 (National Aeronautics and Space Administration ;, 1971), by Sue B. Grafton, Charles E. Libbey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-6051 (National Aeronautics and Space Administration :, 1970), by Robert W. Fulcher, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only) NASA TN D-5921 (National Aeronautics and Space Administration :, 1970), by Joseph R. Chambers, James S. Bowman, Ernie L. Anglin, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-5960 (National Aeronautics and Space Administration, 1970), by E. John Pyle, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-4740 (National Aeronautics and Space Administration ;, 1968), by T.M. Walsh, Dwayne E. Hinton, Jean C. Keating, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Exploratory wind-tunnel investigation of deployable flexible ventral fins for use as an emergency spin-recovery device (National Aeronautics and Space Administration, 1971), by Sanger M. Burk, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-5409 (National Aeronautics and Space Administration :, 1969), by Joseph R. Chambers, Ernie L. Anglin, James S. Bowman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Summary of design considerations for airplane spin-recovery parachute systems (National Aeronautics and Space Administration ;, 1972), by Sanger M. Burk and Langley Research Center (page images at HathiTrust) Summary of spin technology as related to light general-aviation airplanes (National Aeronautics and Space Administration, 1971), by James S. Bowman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-4483 (National Aeronautics and Space Administration ;, 1968), by F. O. Vonbun, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-2656 (National Aeronautics and Space Administration :, 1965), by James S. Bowman and United States National Aeronautics and Space Administration (page images at HathiTrust) A Method of accurately reducing the spin rate of a rotating spacecraft (National Aeronautics and Space Administration :, 1962), by Henry J. Cornille and United States National Aeronautics and Space Administration (page images at HathiTrust) Air-bearing spin facility for measuring energy disspiation (National Aeronautics and Space Administration, 1976), by Robert L. Peterson, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust) NACA wartime reports (Langley Memorial Aeronautical Laboratory, 1942), by A. I. Neihouse, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust) Rotary balance data for an F-15 model with fuel tanks for an angle-of-attack range of 8⁰ to 90⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Billy Barnhart, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust) Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by William Bihrle, Paul Pantason, Billy Barnhart, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust) An investigation in the Langley 20-foot free-spinning tunnel of the spin and recovery characteristics of a 1/30-scale model of the Bell X-2 airplane (National Advisory Committee for Aeronautics, 1949), by Lawrence J. Gale, 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) The Influence of very heavy fuselage mass loadings and long nose lengths upon oscillations in the spin (National Advisory Committee for Aeronautics, 1948), by Ralph W. Stone, Walter J. Klinar, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Spin-tunnel investigation to determine the effectiveness of a rocket for spin recovery (National Advisory Committee for Aeronautics, 1949), by Anshal I. Neihouse, M. S. Uberoi, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Spin-tunnel investigation of the effects of mass and dimensional variations on the spinning characteristics of a low-wing single-vertical-tail model typical of personal-owner airplanes (National Advisory Committee for Aeronautics, 1951), by Walter J. Klinar, Jack H. Wilson, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8ê to 90ê. II, High-wing model C (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Randy S. Hultberg, Waldo Dickens, Julio Chu, Langley Research Center, and Inc Bihrle Applied Research (page images at HathiTrust) Analytical investigation and prediction of spin and recovery characteristics of the North American X-15 airplane (National Aeronautics and Space Administration, 1960), by William D. Grantham, Stanley H. Scher, and Langley Research Center (page images at HathiTrust) The Effect of variations in moments of inertia on spin and recovery characteristics of a single-engine low-wing monoplane with various tail arrangements including a twin tail (National Advisory Committee for Aeronautics, 1948), by Anshal I. Neihouse and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane (National Advisory Committee for Aeronautics, 1951), by William Bihrle and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Effect of spin on aerodynamic properties of bodies of revolution (Aberdeen, Maryland : Aberdeen Proving Ground, 1953., 1953), by L. E. Schmidt, C. H. Murphy, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust) Magnetic spin accelerator (Aberdeen, Maryland : Aberdeen Proving Ground, 1972., 1972), by D. B. Sleator, F. N. Weber, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust) Supersonic wind tunnel magnus measurements of the 7-, 8-, 9- and 10-caliber Army-Navy Spinner Projectile (White Oak, Maryland : United States Naval Ordnance Laboratory, 1968., 1968), by John E. Holmes, Mary Ellen Falusi, Frank J. Regan, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust) Supersonic magnus measurements of the 10-Caliber Army-Navy spinner projectile with wrap-around fins (White Oak, Maryland : United States Naval Ordnance Laboratory, 1970., 1970), by Frank J. Regan, Virginia L. Schermerhorn, and Md.) Naval Ordnance Laboratory (White Oak (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) Criteria for predicting spin susceptibility of fighter-type aircraft (Wright-Patterson Air Force Base, Ohio : Deputy for Engineering, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1972., 1972), by Robert Weissman and United States. Air Force. Systems Command. Aeronautical Systems Division (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) Use of quaternions in flight mechanics (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 Wilbur L. Hankey, Stephen J. Scherr, L. Earl Miller, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust) An analytical study of the dynamics of spinning aircraft. Part I. Flight test data analyses and spin calculations (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by John H. Wykes, Richard A. Collins, Gilbert R. Casteel, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and North American Aviation (page images at HathiTrust) Influence of forebody geometry on aerodynamic characteristics and a design guide for defining departure/spin resistant forebody configurations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), by William Bihrle, E. Dickes, B. Barnhart, Inc Bihrle Applied Research, Wright Research and Development Center, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust) The Dynamics of spinning bodies at large angle of attack (Holloman Air Force Base, New Mexico : Air Force Office of Scientific Research, Directorate of Research Analyses, United States Air Force, 1962., 1962), by J. E. Brunk, R. W. Rakestraw, W. L. Davidson, and United States. Air Force. Office of Scientific Research (page images at HathiTrust) Vortex induced rolling moments on finned missiles at high angle of attack (Boston, Massachusetts : Engineering Laboratories, Boston University, 1968., 1968), by Daniel G. Udelson, United States. |b Air Force. |b Systems Command, Air Force Cambridge Research Laboratories (U.S.), and Boston University (page images at HathiTrust) Correlation of experimental and theoretical steady-state spinning motion for a current fighter airplane using rotation-balance aerodynamic data (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), by T. F. Langham, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust) An analytical study of the dynamics of spinning aircraft. Part II. Wind tunnel tests (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by John H. Wykes, Richard A. Collins, Gilbert R. Casteel, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and North American Aviation (page images at HathiTrust) Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊ I, Low-wing model A (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Randy S. Hultberg, William Mulcay, Langley Research Center, and Inc Bihrle Applied Research (page images at HathiTrust)
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