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ailerons

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View In-flight transport performance optimization By Glenn B. Gilyard

In-flight transport performance optimization

In-flight transport performance optimization

By Glenn B. Gilyard

View Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft By R. H. Stone

Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft

Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft

By R. H. Stone

View Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration By Wendell W. Kelley

Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration

Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration

By Wendell W. Kelley

View Aileron controls for wind turbine applications By Dean R. Miller

Aileron controls for wind turbine applications

Aileron controls for wind turbine applications

By Dean R. Miller

View Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds By Donald Isaacs

Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds

Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds

By Donald Isaacs

View Theoretical study of the rolling response of aircraft to turbulent air By J. K. Zbrozek

Theoretical study of the rolling response of aircraft to turbulent air

Theoretical study of the rolling response of aircraft to turbulent air

By J. K. Zbrozek

View Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls By Langley Aeronautical Laboratory

Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls

Prediction of motions of an airplane resulting from abrupt movement of lateral or directional controls

By Langley Aeronautical Laboratory

View Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap By Langley Aeronautical Laboratory

Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap

Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap

By Langley Aeronautical Laboratory

View Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance By Langley Aeronautical Laboratory

Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance

Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance

By Langley Aeronautical Laboratory

View Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces By Langley Aeronautical Laboratory

Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces

Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces

By Langley Aeronautical Laboratory

View Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil By Langley Aeronautical Laboratory

Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

By Langley Aeronautical Laboratory

View Study of the effects of radii of gyration and altitude on aileron effectiveness at high speed By Langley Aeronautical Laboratory

Study of the effects of radii of gyration and altitude on aileron effectiveness at high speed

Study of the effects of radii of gyration and altitude on aileron effectiveness at high speed

By Langley Aeronautical Laboratory

View Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane By Langley Aeronautical Laboratory

Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane

Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane

By Langley Aeronautical Laboratory

View Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed By Langley Aeronautical Laboratory

Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed

Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed

By Langley Aeronautical Laboratory

View Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron By Langley Aeronautical Laboratory

Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron

Comparison of pitching moments produced by plain flaps and by spoilers and some aerodynamic characteristics of an NACA 23012 airfoil with various types of aileron

By Langley Aeronautical Laboratory

View Analysis of available data on the effectiveness of ailerons without exposed overhang balance By Langley Aeronautical Laboratory

Analysis of available data on the effectiveness of ailerons without exposed overhang balance

Analysis of available data on the effectiveness of ailerons without exposed overhang balance

By Langley Aeronautical Laboratory

View Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application By G. M. Gregorek

Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application

Comparison of pressure distributions on model and full-scale NACA 64-621 airfoils with ailerons for wind turbine application

By G. M. Gregorek

View Tables of the aerodynamic aileron-coefficients for an oscillating wing-aileron system in a subsonic, compressible flow By E. M. De Jager

Tables of the aerodynamic aileron-coefficients for an oscillating wing-aileron system in a subsonic, compressible flow

Tables of the aerodynamic aileron-coefficients for an oscillating wing-aileron system in a subsonic, compressible flow

By E. M. De Jager

View Reynolds number effects on the performance of lateral control devices By Raymond E. Mineck

Reynolds number effects on the performance of lateral control devices

Reynolds number effects on the performance of lateral control devices

By Raymond E. Mineck

View Aileron controls for wind turbine applications By Dean R Miller

Aileron controls for wind turbine applications

Aileron controls for wind turbine applications

By Dean R Miller

View Description of an experimental (hydrogen peroxide) rocket system and its use in measuring aileron and rudder effectiveness of a light airplane By

Description of an experimental (hydrogen peroxide) rocket system and its use in measuring aileron and rudder effectiveness of a light airplane

Description of an experimental (hydrogen peroxide) rocket system and its use in measuring aileron and rudder effectiveness of a light airplane

By

View Summary of NASA/DOE aileron-control development program for wind turbines By Dean R. Miller

Summary of NASA/DOE aileron-control development program for wind turbines

Summary of NASA/DOE aileron-control development program for wind turbines

By Dean R. Miller

View Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6 By Charles B Johnson

Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6

Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6

By Charles B Johnson

View Feasibility study of aileron and spoiler control systems for large horizontal axis wind turbines By

Feasibility study of aileron and spoiler control systems for large horizontal axis wind turbines

Feasibility study of aileron and spoiler control systems for large horizontal axis wind turbines

By