Explore Books on
leading edges (aerodynamics)

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

By E. Richard White

Leading-edge slat optimization for maximum airfoil lift

By Lawrence E. Olson

Fluid-thermal-structural study of aerodynamically heated leading edges

By Pramote Dechaumphai

Study of supersonic wings employing the attainable leading-edge thrust concept

By W. D. Middleton

Navier-Stokes analysis of airfoils with leading edge ice accretions

By Mark G. Potapczuk

Leading-edge receptivity for blunt-nose bodies

By F. W. Hammerton

Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44 ̊swept wing

By William P. Henderson

Leading-edge deflection optimization for a highly swept arrow-wing configuration

By Paul L. Coe

Estimation of leading-edge thrust for supersonic wings of arbitrary planform

By Harry W. Carlson

Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing

By Samuel J. Scott

Leading-edge receptivity for blunt-nose bodies

By E. J. Kerschen

Leading-edge deflection optimization for a highly swept arrow-wing configuration

By Paul L Coe

Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2

By E. Ann Bare

Estimation of attainable leading-edge thrust for wings at subsonic and supersonic speeds

By Harry W. Carlson

Rolling maneuver load alleviation using active controls

By Jessica A. Woods-Vedeler

Fluid flow and heat convection studies for actively cooled airframes

By Anthony F. Mills

Fluid flow and heat convection studies for actively cooled airframes, May 1992 - October 1992

By Anthony F. Mills

Leading-edge slat optimization for maximum airfoil lift

By Lawrence E Olson

Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44ê swept wing

By William P Henderson

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

By H. Paul Stough

The leading edge problem according to the Krook model

By Robert Walter Clark

A theoretical investigation for delta wings with leading-edge separation at low speeds

By R. K. Nangia

Specification for a Program for an Interative Aeroelastic Solution (PIAS)

By

Surface-pressure and flow-visualization data at mach number 1.60 for three 65p0s delta wings varying in leading-edge radius and camber

By