1-24 of 27 Books
In-flight transport performance optimization
In-flight transport performance optimization
By Glenn B. Gilyard
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
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
Aileron controls for wind turbine applications
Aileron controls for wind turbine applications
By Dean R. Miller
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
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
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
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
Development of an advanced composite aileron for the L-1011 transport aircraft
Development of an advanced composite aileron for the L-1011 transport aircraft
By C. F. Griffin
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
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
Force and pressure tests on the GA(W)-1 airfoil with a 20 % aileron and pressure tests with a 30 % Fowler flap
Force and pressure tests on the GA(W)-1 airfoil with a 20 % aileron and pressure tests with a 30 % Fowler flap
By W. H. Wentz
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
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
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
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
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
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
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
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
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
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
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
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