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Stability of airplanes, Lateral -- Testing

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• Stability of airplanes, Lateral
• Stability of airplanes -- Testing
• Airplanes -- Testing
• Testing

• Yawing (Aerodynamics) -- Testing
• Stability of airplanes, Lateral -- Measurement -- Equipment and supplies -- Testing

• NASA TR R-65 (National Aeronautics and Space Administration ;, 1960), by Clarence L. Gillis, Charles T. D'Aiutolo, Jesse L. Mitchell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed measurements of oscillatory lateral stability derivatives of a model of 60 degree delta-wing bomber (National Aeronautics and Space Administration, 1959), by John W. Paulson and Langley Research Center (page images at HathiTrust)
• Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design (National Aeronautics and Space Administration, 1961), by Odell A. Morris, Gerald V. Foster, and Langley Research Center (page images at HathiTrust)
• Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds (National Aeronautics and Space Administration, 1960), by Walter B. Olstad and Langley Research Center (page images at HathiTrust)
• Investigation of the aerodynamic characteristics of a 0.067-scale model of the x-15 airplane (configuration 3) at mach numbers of 2.29, 2.98, and 4.65 (National Aeronautics and Space Administration, 1959), by Arthur E. Franklin, Robert M. Lust, and Langley Research Center (page images at HathiTrust)
• Research on blunt-faced entry configurations at angles of attack Between 60° and 90° (National Aeronautics and Space Administration, 1960), by William H. Phillips and Langley Research Center (page images at HathiTrust)
• Stability and control characteristics at low subsonic speeds of an airplane configuration having two types of variable-sweep wings (National Aeronautics and Space Administration, 1960), by Bernard Spencer and Langley Research Center (page images at HathiTrust)
• Investigation of the low-subsonic aerodynamic characteristics of a model of a modified lenticular reentry configuration (National Aeronautics and Space Administration, 1962), by George M. Ware and Langley Research Center (page images at HathiTrust)

• Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40©� sweepback (National Advisory Committee for Aeronautics, 1958), by Charles T. D'Aiutolo, Homer P. Mason, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)

• Operational and performance characteristics of the X-15 spherical, hypersonic flow-direction sensor (National Aeronautics and Space Administration ;, 1965), by Chester H. Wolowicz, Terrence D. Gossett, and Flight Research Center (U.S.) (page images at HathiTrust)

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

• Flight text of an autopilot installation as a lateral gust alleviator in a PT-26 airplane. (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1956), by Charles Chalk (page images at HathiTrust)
• Comparison of aerodynamic stability derivatives obtained from analysis of F-100A dynamic lateral flight test data by two least squares methods. (Cornell Aeronautical Laboratory, Inc., 1959), by Norman E. Gowin (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)
• Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Michael J. Mann, Charles H. Fox, Jarrett K. Huffman, and Langley Research Center (page images at HathiTrust)
• Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Dale R. Satran, Ernie L. Anglin, William P. Gilbert, and Langley Research Center (page images at HathiTrust)
• Relative control effectiveness technique with application to airplane control coordination (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Frederick J. Lallman and Langley Research Center (page images at HathiTrust)
• Recent progress towards predicting aircraft ground handling performance (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Thomas J. Yager, Ellis J. White, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effects of external stores on the aerodynamic characteristics of a 60 ̊Delta-wing fighter model at mach 1.60 to 2.87 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by M. Leroy Spearman, William J. Monta, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by A. B. Blair, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 ̊ (National Aeronautics and Space Administration ;, 1974), by William P. Henderson, Jarrett K. Huffman, and Langley Research Center (page images at HathiTrust)
• Aerodynamic roll damping of a T-tail transport configuration (National Aeronautics and Space Administration ;, 1974), by Richmond P. Boyden and Langley Research Center (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)
• Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Jay M. Brandon and Langley Research Center (page images at HathiTrust)
• Simulator evaluation of separation of display parameters in path-following tasks (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Garimella R. Sarma, James J. Adams, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Jack D. Stephenson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Turbulence and lateral-directional flying qualities (For sale by the National Technical Information Service, 1971), by James A. Franklin, United States National Aeronautics and Space Administration, and Princeton University (page images at HathiTrust)
• An in-flight simulation of lateral control nonlinearities (National Aeronautics and Space Administration ;, 1975), by David R. Ellis, Narayan W. Tilak, Langley Research Center, and Princeton University. Flight Research Laboratory (page images at HathiTrust)
• Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David G. Mitchell, David H. Klyde, Bimal L. Aponso, Dryden Flight Research Facility, Inc PRC, and inc Systems Technology (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)
• Subsonic roll-damping characteristics of a series of wings (National Aeronautics and Space Administration ;, 1974), by Richmond P. Boyden and Langley Research Center (page images at HathiTrust)
• A theoretical analysis of the dynamic lateral stability and control of a parawing vehicle (National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1966), by Joseph R. Chambers and Peter C. Boisseau (page images at HathiTrust; US access only)
• Static lateral characteristics at high subsonic speeds of a complete airplane model with a highly tapered wing having the 0.80 chord line unswept and with several tail configuration. (National Aeronautics and Space Administration, 1961), by Kenneth W. Goodson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration (National Aeronautics and Space Administration ;, 1974), by Blair B. Gloss and Langley Research Center (page images at HathiTrust)
• An analytical study of aircraft lateral-directional handling qualities using pilot models (National Aeronautics and Space Administration ;, 1976), by James J. Adams, Frederick L. Moore, and Langley Research Center (page images at HathiTrust)
• Computed lateral rate and acceleration power spectral response of conventional and STOL airplanes to atmospheric turbulence (National Aeronautics and Space Administration ;, 1975), by Jacob H. Lichtenstein and Langley Research Center (page images at HathiTrust)
• Lateral aerodynamic parameters extracted from light data for the F-8C airplane in maneuvering flight (Natural Aeronautics and Space Administration :, 1977), by William T. Suit and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack (National Aeronautics and Space Administration ;, 1977), by James M. Luckring and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Extraction from flight data of lateral aerodynamic coefficients for F-8 aircraft with supercritical wing (National Aeronautics and Space Administration ;, 1974), by James L. Williams, William T. Suit, and Langley Research Center (page images at HathiTrust)
• Investigation of lateral-directional dynamic stability of a tilt-wing V/STOL transport (National Aeronautics and Space Administration :, 1970), by Joseph R. Chambers, Sue B. Grafton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Lateral static and dynamic aerodynamic parameters of the Kestrel aircraft (XV-6A) extracted from flight data (National Aeronautics and Space Administration ;, 1974), by William T. Suit, James L. Williams, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of static longitudinal and lateral characteristics of a full-scale mockup of a light single-engine high-wing airplane (National Aeronautics and Space Administration ;, 1973), by H. Douglas Greer and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a three-engine supersonic transport model having a low-aspect-ratio variable-sweep warped wing (National Aeronautics and Space Administration, 1964), by Odell A. Morris, Dennis E. Fuller, and Langley Research Center (page images at HathiTrust)
• Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails (National Aeronautics and Space Administration, 1964), by Vernard E. Lockwood, Wilson E. Thompson, and Langley Research Center (page images at HathiTrust)
• Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1.57, 2.14, 2.54, and 2.87 (National Aeronautics and Space Administration, 1960), by Arthur E. Franklin, Robert M. Lust, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of a tailless fixed-wing supersonic transport configuration at Mach number 2.20 (National Aeronautics and Space Administration, 1964), by Gerald V. Foster, William A. Corlett, and Langley Research Center (page images at HathiTrust)
• The lateral and directional aerodynamic characteristics of a re-entry configuration based on a blunt 13 degree half cone at Mach numbers to 0.90 (National Aeronautics and Space Administration, 1961), by George C. Kenyon and Ames Research Center (page images at HathiTrust)
• Low-speed investigation of the aerodynamic characteristics of a variable-sweep supersonic transport configuration having a blended wing and body (National Aeronautics and Space Administration, 1961), by William C. Sleeman, A. Warner Robins, and Langley Research Center (page images at HathiTrust)
• Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels (National Aeronautics and Space Administration, 1961), by M. Leroy Spearman, Gerald V. Foster, and Langley Research Center (page images at HathiTrust)
• Longitudinal and lateral stability characteristics of two four-jet vtol models in the transition speed range (National Aeronautics and Space Administration, 1965), by Raymond D. Vogler, Richard E. Kuhn, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pilot-model measurements of pilot responses in a lateral-directional control task (National Aeronautics and Space Administration :, 1976), by James J. Adams and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack (National Aeronautics and Space Administration ;, 1974), by Paul L. Coe, William A. Newsom, and Langley Research Center (page images at HathiTrust)
• Low-speed effects of high-lift devices on the aerodynamic characteristics of a supersonic transport model with outboard tails (National Aeronautics and Space Administration, 1963), by William C. Sleeman, Paul G. Fournier, Edward J. Ray, and Langley Research Center (page images at HathiTrust)
• Flight evaluation of the effects of leading-edge-slat span on the stability and control characteristics of a swept-wing fighter-type airplane during accelerated longitudinal maneuvers at transonic speeds (National Advisory Committee for Aeronautics, 1958), by Gene J. Matranga, Katharine H. Armistead, Flight Research Center (U.S.), and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Theoretical analysis of the rolling motions of aircraft using a flicker-type automatic roll stabilization system having a displacement-plus-rate response (National Advisory Committee for Aeronautics, 1949), by Howard J. Curfman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Investigation of the dynamic lateral stability and control characteristics of a model of a fighter airplane without a horizontal tail and equipped with either single or twin vertical tails (National Advisory Committee for Aeronautics, 1949), by John W. Draper, Robert W. Rose, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Low-speed static lateral stability characteristics of a canard model having a 60©� triangular wing and horizontal tail (National Advisory Committee for Aeronautics, 1949), by William R. Bates, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Low-speed wind-tunnel investigation of jet control on a 35©� swept wing (National Advisory Committee for Aeronautics, 1953), by John G. Lowry, Thomas R. Turner, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Investigation of the aerodynamic characteristics in pitch and sideslip of a 45©� swept-wing airplane configuration with various vertical locations of the wing and horizontal tail. Static lateral and directional stability; Mach numbers of 1.41 and 2.01 (National Advisory Committee for Aeronautics, 1957), by M. Leroy Spearman, Ross B. Robinson, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States. National Advisory Committee for Aeronautics (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)
• Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing (National Advisory Committee for Aeronautics, 1958), by Edward C. Polhamus, Kenneth P. Spreemann, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60©� delta-wing airplane model (National Advisory Committee for Aeronautics, 1958), by Lewis R. Fisher, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. Aspect-ratio series (National Advisory Committee for Aeronautics, 1953), by Paul G. Fournier, Andrew L. Byrnes, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Aerodynamic loading characteristics in sideslip of a 45©� sweptback wing with and without a fence at high subsonic speeds (National Advisory Committee for Aeronautics, 1955), by Richard E. Kuhn, Andrew L. Byrnes, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Damping in roll of models with 45©�, 60©�, and 70©� delta wings determined at high subsonic, transonic, and supersonic speeds with rocket -powered models (National Advisory Committee for Aeronautics, 1952), by E. Claude Sanders, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Experimental determination of effect of structural rigidity on rolling effectiveness of some straight and swept wings at Mach numbers from 0.7 to 1.7 (National Advisory Committee for Aeronautics, 1950), by H. Kurt Strass, Paul E. Purser, E. M. Fields, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Subsonic flight investigation of methods to improve the damping of lateral oscillations by means of a viscous damper in the rudder system in conjunction with adjusted hinge-moment parameters (National Advisory Committee for Aeronautics, 1954), by Harold L. Crane, John M. Elliott, George J. Hurt, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Effect of airfoil profile of symmetrical sections on the low-speed rolling derivatives of 45©� sweptback-wing models of aspect ratio 2.61 (National Advisory Committee for Aeronautics, 1949), by William Letko, Jack D. Brewer, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• A theoretical analysis of the effect of time lag in an automatic stabilization system on the lateral oscillatory stability of an airplane (National Advisory Committee for Aeronautics, 1950), by Leonard Sternfield, Ordway B. Gates, 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)
• 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)
• The effects of mass distribution on the low-speed dynamic lateral stability and control characteristics of a model with a 45©� sweptback wing (National Advisory Committee for Aeronautics, 1951), by Donald E. Hewes and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight investigation of the effect of control centering springs on the apparent spiral stability of a personal-owner airplane (National Advisory Committee for Aeronautics, 1951), by James B. Whitten, Donald E. Hewes, Paul A. Hunter, John P. Campbell, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Properties of honeycomb cores as affected by fiber type, fiber orientation, resin type, and amount (National Advisory Committee for Aeronautics, 1951), by R. J. Seidl, A. W. Voss, D. J. Fahey, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives (National Advisory Committee for Aeronautics, 1952), by Robert O. Schade, James L. Hassell, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Static stability characteristics of three thick wing models with parabolic plan forms at mach number of 3.11 (National Aeronautics and Space Administration, 1959), by M. J. Queijo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed measurements of oscillatory lateral stability derivatives of a 1/7-scale model of the North American X-15 airplane (National Aeronautics and Space Administration, 1959), by John W. Paulson, James L. Hassell, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation of the static and dynamic-rotary stability derivatives of a flat-top wing-body model at Mach numbers of 2.5, 3.0 and 3.5 (National Aeronautics and Space Administration, 1960), by Bedford A. Lampkin, Kenneth C. Endicott, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed static longitudinal and lateral stability characteristics of a variable-incidence delta-wing canard model with high-lift canard surfaces (National Aeronautics and Space Administration, 1959), by Clarence D. Cone and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics of a spoiler-slot-deflector control on a 45° sweptback-wing-fuselage model at high subsonic speeds (National Aeronautics and Space Administration, 1960), by Alexander D. Hammond and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static stability characteristics of a series of hypersonic boost-glide configurations at mach numbers of 1.41 and 2.01 (National Aeronautics and Space Administration, 1959), by Gerald V. Foster and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3 (National Advisory Committee for Aeronautics, 1959), by M. Leroy Spearman, Arthur Henderson, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds (National Advisory Committee for Aeronautics, 1956), by Percy J. Bobbitt, Kenneth Margolis, Frank S. Malvestuto, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds (National Advisory Committee for Aeronautics, 1956), by Arthur Henderson and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Wind-tunnel investigation of effects of ventral fins at two positions on lateral-stability derivatives of 45©� high-wing model oscillating in yaw (National Advisory Committee for Aeronautics, 1957), by Byron M. Jaquet 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, 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 John G. Lowry, Thomas A. Toll, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6©� and NACA 65A006 airfoil section (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), by Harold S. Johnson, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of aspect ratio on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with flap and with retractable ailerons (U.S. Government Printing Office, 1952), by William M. O'Hare, John R. Hagerman, Rodger L. Naeseth, Jack Fischel, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lateral stability of an F-100A airplane (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1957., 1957), by Norman E. Gowin, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (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)
• A flight investigation of lateral-directional handling qualities for V/STOL aircraft in low speed maneuvering flight (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by K. H. Doetsch, D. M. McGregor, D. G. Gould, Air Force Flight Dynamics Laboratory (U.S.), and National Aeronautical Establishment (Canada) (page images at HathiTrust)

More items available under broader and related terms at left.