Method for Caluculating Lift Distributions for Unswept Wings with Flaps or Ailerons by use of Nonlinear Section Lift Data
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DAMPING DERIVATIVES - STABILITY↗
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Results for “AILERONS - DEFLECTION”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Experimental Investigations of Rolling Performance of Straight and Sweptback Flexible Wings with Various Ailerons
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Cole, Henry A↗
Calculations on the Forces and Moments for an Oscillating Wing-aileron Combination in Two-dimensional Potential Flow at Sonic Speed
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Nelson, Herbert C↗
Rolling effectiveness and aileron reversal of rectangular wings at supersonic speeds
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Hedgepeth, John M↗
A calculation study of wing-aileron flutter in two degrees of freedom for two-dimensional supersonic flow
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Woolston, Donald S↗
Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device for Personal Airplanes
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Phillips, William H↗
Lift and moment coefficients for an oscillating rectangular wing-aileron configuration in supersonic flow
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Berman, Julian H↗
Some Wind-tunnel Experiments on Single-degree-of-freedom Flutter of Ailerons in the High Subsonic Speed Range
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Clevenson, Sherman A↗
Preliminary free-flight investigation of the effect of airfoil section on aileron rolling effectiveness at transonic and supersonic speeds
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Sandahl, Carl A↗
Preliminary investigation at a Mach number of 1.9 and a Reynolds number of 2,200,000 of three ailerons applicable to the Bell XS-2 airplane design
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Sivells, James C↗
Free-flight Investigation at Transonic and Supersonic Speeds of a Wing-aileron Configuration Simulating the D-558-2 Airplane
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Sandahl, Carl A↗
Free-flight Investigation of the Rolling Effectiveness of Several Delta Wing : Aileron Configurations at Transonic and Supersonic Speeds
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Sandahl, Carl A↗
Preliminary Investigation of Various Ailerons on a 42 Degree Sweptback Wing for Lateral Control at Transonic Speeds
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Turner, Thomas R↗
Wind-tunnel Investigation of Transonic Aileron Flutter of a Semispan Wing Model with an NACA 23013 Section
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Perone, Angelo↗
An Investigation at Low Speed of a 51.3 Degrees Sweptback Semispan Wing with a Raked Tip and with 16.7-percent-chord Ailerons Having Three Spans and Three Trailing-edge Angles
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Schneiter, Leslie E↗
Free-flight Investigation of the Rolling Effectiveness at High Subsonic, Transonic, and Supersonic Speeds of Leading-edge and Trailing-edge Ailerons in Conjunction with Tapered and Untapered Plan Forms
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Strass, H Kurt↗
Aerodynamic Characteristics at Subsonic and Transonic Speeds of a 42.7 Degree Sweptback Wing Model Having an Aileron with Finite Trailing-edge Thickness
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Lockwood, Vernard E↗
Wind-tunnel Investigation at Low Speeds of Various Plug-aileron and Lift-flap Configurations on a 42 Degree Sweptback Semispan Wing
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Schneiter, Leslie E↗