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Discover Leading Edges (Aerodynamics)
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Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2
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Estimation of leading-edge thrust for supersonic wings of arbitrary planform
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Exploratory investigation of the effects of blowing from the leading edge of a delta wing
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Fluid flow and heat convection studies for actively cooled airframes
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The oscillating jet flap
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The pressure drag of an aerofoil with six different round leading edges, at transonic and low supersonic speeds
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Estimation of attainable leading-edge thrust for wings at subsonic and supersonic speeds
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Estimation of attainable leading-edge thrust for wings at subsonic and supersonic speeds
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Leading-edge slat optimization for maximum airfoil lift
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The leading edge problem according to the Krook model
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Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50p0s to 74p0s delta wings on common fuselage
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Study of supersonic wings employing the attainable leading-edge thrust concept
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Leading-edge slat optimization for maximum airfoil lift
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Navier-Stokes analysis of airfoils with leading edge ice accretions
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A theoretical investigation for delta wings with leading-edge separation at low speeds
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Flight investigation of the effects of an outboard wing-leading-edge modification on stall/spin characteristics of a low-wing, single-engine, T-tail light airplane
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Leading-edge receptivity for blunt-nose bodies
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Visualization of leading edge vortices on a series of flat plate delta wings
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Leading-edge deflection optimization for a highly swept arrow-wing configuration
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Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing
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Supersonic wings with significant leading-edge thrust at cruise
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Wind-tunnel investigation of effects of wing-leading-edge modifications on the high angle-of-attack characteristics of a T-tail low-wing general-aviation aircraft
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Rolling maneuver load alleviation using active controls
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Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing
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