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Inaeronautics, aflexible wing is anairfoil or aircraft wing which can deform in flight.
Early pioneer aeroplanes such as the 1903Wright Flyer used the flexible characteristics of lightweight construction to control flight throughwing warping. Others made collapsible wings for folding away, such as theflying car designs byGustave Whitehead.
Since the 1960s flexible wings have dominatedhang glider andultralight aircraft designs, with such types as the delta-shapedRogallo wing and the fully collapsibleparaglider.
More recently, the advent of high-strength flexible materials and other advanced technologies has renewed interest in the use of flexing for control purposes.
The first effective control system on a powered aircraft allowed one to fly for the first time. TheWright Flyer usedwing warping for lateral or roll control, by twisting one wing tip to increase its angle to the air while twisting the other to reduce its angle. TheWright brothers patented system was widely copied.
However, as engine powers and air speeds rose, so too did the forces needed to operate the pilot controls and by 1914 warping was all but abandoned.
Predating successful controlled and powered flight, collapsible wings had been developed in an attempt to solve the problems of ground storage and transport. A system of radial ribs like a giantfolding fan, sometimes described as bat-like, was used by some pioneers, notablyGustave Whitehead in his attempts to build aflying car.
Aeroelasticity is the natural tendency of any wing to flex under aerodynamic and inertial loads while in flight. Most designs seek to minimise the effects by making the wing structure as stiff as possible. However some have sought to use the effect to advantage.
A relatively early example is provided by the flying-wing gliders of theHorten brothers during the 1930s, whose wing tips flexed upwards in flight to act as stabilising surfaces.
The advent of the jet engine andtransonic flight speeds brought a sharp increase in aerodynamic forces, made worse by the innate structural inefficiency of theswept wing, with the combination leading to dangerous characteristics in extreme flight conditions. The aeroisoclinic wing, developed byGeoffrey T. R. Hill in the 1950s and flown on theShort SB.4 Sherpa, was an attempt control the flexing in such a way as to maintain handling characteristics in all flight regimes. Similaraeroelastic tailoring was later applied to experimentalforward-swept wings, where it is a necessity for any safe design.
In 1948 the husband-and-wife team ofFrancis andGertrude Rogallo developed a flexible kite which could be collapsed for storage. A key part of their design is the mixed use of tension lines and aerodynamic forces to stabilise and control the wing. The wing remains a constant shape in flight under wind pressure, and the lines are used to control its position.
Over the following years they developed the design and then Francis, working at NASA's Langley research centre, further developed the concept into proposals for crewed aircraft such as a space vehicle re-entry system.
Following a series of talks in 1959 and 1960 his ideas spread rapidly and two designs in particular, the Rogallo delta and the paraglider, were soon being used for kites, hang gliders and ultralight aircraft. Types with an engine backpack for the pilot are known as powered gliders. Although tested for spacecraft descent, no Rogallo types have been used by NASA.
Francis Rogallo evolved his trademark double-delta "parawing" during the 1950s. Unlike the earlier kites it uses several struts to maintain its planform, while still relying on air pressure from beneath to develop its conical upper profile.
Like the original Rogallo kites, the parafoil is fully collapsible. But unlike them it is double-skinned. Comprising an open-fronted aerofoil wing, it is held in shape by the pressure of air from in front. Many flexible ribs are needed to hold its aerofoil shape.
In the 21st. century, new materials possessing both flexibility and strength are being experimented with, in order to merge control surfaces into the main wing surface.[1][2] For example, a flexiblewing flap has been test flown on aGulfstream III.[3] Flexible aerofoils and control surfaces operate by regular deformation of the wing material. Current challenges are centred around deforming the material to manipulate aerodynamic loads without exceeding the materials elastic limit.[4]
The key benefits of flexible aerofoils are the reductions in aerodynamic drag.[5] Current flight control mechanisms operate using hinges, which significantly disrupt the airflow and even generate vortices between the control surface and wing boundary. A flexible aerofoil can smoothly alter its shape to deflect the airflow, allowing the aerodynamic forces to be controlled without creating 'gaps' between hinges.[6]
For smaller craft, the increasing sophistication of smart control systems is being combined with flexible technologies to create articulated wings which mimic the natural flexing of birds' wings in flight. It is now even practicable to use a bird-like flapping action to provide thrust as anornithopter. TheUTIAS Snowbird ornithopter of 2010 was human-powered.
The technology has been given various names, such as the morphing wing, smart airfoil oradaptive compliant wing.