Pressure-Distribution Measurements of a Low-Drag Airfoil with Slotted Flap Submitted by Curtiss-Wright Corporation
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PRESSURE DISTRIBUTION - WINGS - CURTISS P-60A-WING↗
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Results for “flaps”
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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Two-dimensional Wind-tunnel Investigation of Spoiler Aileron Flap Model for the Hughes XF-11 Airplane
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WING SPOILERS, RETRACTABLE↗
A Flight Investigation of Internally Balanced Sealed Ailerons in the Presence of a Balanced Split Flap
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AILERONS - DEFLECTION↗
Flight Tests of Dive-recovery Flaps on an XP-51 Airplane
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WING FLAPS - NACA↗
Wind-tunnel investigation of the effects of surface-covering distortion on the characteristics of a flap having undistorted contour maintained for various distances ahead of the trailing edge
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CONTROL STICKS - FORCES↗
Wind-tunnel investigation of an NACA 0009 airfoil with 0.25-and 0.50-airfoil-chord plain flaps tested independently and in combination
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CONTROL SURFACES, SEALED-GAP↗
Effect of landing flaps and landing gear on the spin and recovery characteristics of airplanes
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WIND TUNNEL TESTS - NACA - FREE-SPINNING (15') WOR↗
Wind-tunnel investigation of boundary-layer control by suction on NACA 655-424 airfoil with double slotted flap
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WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENC↗
Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50- airfoil chord plain sealed flaps
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CONTROL SURFACES, BALANCED - SEALED-GAP↗
Low-speed Investigation of the Stalling of a Thin, Faired, Double-wedge Airfoil with Nose Flap
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AIRFOILS, WEDGE - DOUBLE - CHAR & MOMENTS↗
Theoretical analysis of oscillations in hovering of helicopter blades with inclined and offset flapping and lagging hinge axes
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ROTOR BLADES - FLAPPING↗
Estimation of low-speed lift and hinge-moment parameters for full-span trailing-edge flaps on lifting surfaces with and without sweepback
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TAIL SURFACES, SWEPTBACK - CHARACTERISTICS↗
Some theoretical characteristics of trapezoidal wings in supersonic flow and a comparison of several wing-flap combinations
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WINGS, TRAPEZOIDAL - CHARACTERISTICS, EFFECT OF CO↗
Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds
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CONTROLS - COMPLETE WINGS↗
Measurements in Flight of the Lateral-Control Characteristics of an Airplane Equipped with Full-Span Zap Flaps and Simple Circular-Arc-Type Ailerons
Flight tests were conducted on the OS2U-2 seaplane with simple circular-arc-type ailerons directly connected to the actuating torque tube. Two aileron test installations were made, differing only in the inclination of the projecting surface with the wing's upper surface. The lateral-control characteristics of the airplane were determined from data obtained in stalls and rudder-fixed aileron rolls. The revised ailerons were deficient in maximum rolling effectiveness, but were capable of controlling the rolling tendencies of the airplane near the stall.
AILERON CONTROLS - VOUGHT OS2U-2↗
Power-On Wind-Tunnel Tests of the 1/8-Scale Model of the Brewster F2A Airplane with Full-span Slotted Flaps
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WING FLAPS, SLOTTED & AILERONS, SLOT-LIP↗
Power-On Longitudinal-Stability and Control Tests of the 1/8-scale Model of the Brewster F2A Airplane Equipped with Full-Span Slotted Flaps and a New Horizontal Tail
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WING FLAPS, SLOTTED - FULL-SPAN↗
Measurements in Flight of the Stability, Lateral Control, and Stalling Characteristics of an Airplane Equipped with Full-span Zap Flaps and Spoiler-Type Ailerons
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STABILITY & CONTROL - VOUGHT-SIKORSKY OS2U-2↗