Jump to content

Wing: Difference between revisions

From Wikipedia, the free encyclopedia
Content deleted Content added
m fixed lint errors – file options; thumbnails shouldn't be used in galleries
Line 1: Line 1:
{{Short description|Appendage used for flight}}
{{Short description|Appendage used for flight}}
{{Other uses|Wing (disambiguation)|Wings (disambiguation)}}
{{Other uses|Wing (disambiguation)|Wings (disambiguation)}}
[[File:Dead Pica pica 10-right wing inside.JPG|thumb|Wing of a [[Eurasian magpie]], which allows flight by the flapping of wings.]]
[[File:Dead Pica pica 10-right wing inside.JPG|thumb|Wing of a [[Eurasian magpie]], which allows flight by the flapping of wings]]
[[File:wing.two.arp.600pix.jpg|thumb|right|A [[swept wing]] [[KC-10 Extender]] (top) [[air-to-air refueling|refuel]]s a trapezoidal-wing [[F-22 Raptor]].]]
[[File:wing.two.arp.600pix.jpg|thumb|right|A [[swept wing]] [[KC-10 Extender]] (top) [[air-to-air refueling|refuel]]s a trapezoidal-wing [[F-22 Raptor]]]]


A '''wing''' is a type of [[fin]] that produces [[Lift (force)|lift]] while moving through air or some other [[fluid]]. Accordingly, wings have [[Streamlines, streaklines, and pathlines|streamlined]] [[Cross section (geometry)|cross-sections]] that are subject to [[aerodynamic force]]s and act as [[airfoil]]s. A wing's [[Aerodynamics|aerodynamic]] efficiency is expressed as its [[lift-to-drag ratio]]. The lift a wing generates at a given speed and [[angle of attack]] can be one to two [[order of magnitude|orders of magnitude]] greater than the total [[drag (physics)|drag]] on the wing. A high lift-to-drag ratio requires a significantly smaller [[thrust]] to propel the wings through the air at sufficient lift.
A '''wing''' is a type of [[fin]] which produces [[Lift (force)|lift]] while moving through air or some other [[fluid]]. Accordingly, wings have [[Streamlines, streaklines, and pathlines|streamlined]] [[Cross section (geometry)|cross-sections]] which are subject to [[aerodynamic force]]s and act as [[airfoil]]s. A wing's [[Aerodynamics|aerodynamic]] efficiency is expressed as its [[lift-to-drag ratio]]. The lift a wing generates at a given speed and [[angle of attack]] can be one to two [[order of magnitude|orders of magnitude]] greater than the total [[drag (physics)|drag]] on the wing. A high lift-to-drag ratio requires a significantly smaller [[thrust]] to propel the wings through the air at sufficient lift.


Lifting structures used in water include various [[Foil (fluid mechanics)|foils]], such as [[hydrofoil]]s. [[Hydrodynamics]] is the governing science, rather than aerodynamics. Applications of underwater foils occur in [[Hydroplane (boat)|hydroplane]]s, [[sailboat]]s and [[submarine]]s.
Lifting structures used in water include various [[Foil (fluid mechanics)|foils]] like [[hydrofoil]]s. [[Hydrodynamics]] is the governing science, rather than aerodynamics. Applications of underwater foils occur in [[Hydroplane (boat)|hydroplane]]s, [[sailboat]]s, and [[submarine]]s.


==Etymology and usage==
==Etymology and usage==
For many centuries, the word "wing", from the Old Norse ''vængr'',<ref>{{cite web|url=http://www.etymonline.com/index.php?term=wing|title=Online Etymology Dictionary|publisher=Etymonline.com|access-date=2012-04-25}}</ref> referred mainly to the foremost [[limb (anatomy)|limb]]s of [[bird]]s (in addition to the architectural aisle). But in recent centuries the word's meaning has extended to include lift producing appendages of [[insect wing|insect]]s, [[bat]]s, [[pterosaur]]s, [[boomerang]]s, [[Wingsail|some sail boats]] and [[aircraft]], or the [[Glossary_of_motorsport_terms#W|
For many centuries, the word "wing", from the Old Norse ''vængr'',<ref>{{cite web|url=http://www.etymonline.com/index.php?term=wing|title=Online Etymology Dictionary|publisher=Etymonline.com|access-date=2012-04-25}}</ref> referred mainly to the foremost [[limb (anatomy)|limb]]s of [[bird]]s (in addition to the architectural aisle). But in recent centuries the word's meaning has extended to include lift producing appendages of [[insect wing|insect]]s, [[bat]]s, [[pterosaur]]s, [[boomerang]]s, [[Wingsail|some sail boats]], and [[aircraft]] or the [[Glossary_of_motorsport_terms#W|
inverted airfoil]] on a [[automobile racing|race car]] that generates a [[downforce|downward force]] to increase traction.
inverted airfoil]] on a [[automobile racing|race car]] which generates a [[downforce|downward force]] to increase traction.


==Aerodynamics==
==Aerodynamics==
[[File:Cloud over A340 wing.JPG|thumb|right|Condensation in the low pressure region over the wing of an [[Airbus A340]], passing through humid air.]]
[[File:Cloud over A340 wing.JPG|thumb|right|Condensation in the low pressure region over the wing of an [[Airbus A340]], passing through humid air]]
[[File:Aircraft flaps.svg|thumb|right|[[flap (aircraft)|Flaps]] (green) are used in various configurations to increase the wing area and to increase the lift. In conjunction with [[spoiler (aeronautics)|spoilers]] (red), flaps maximize drag and minimize lift during the landing roll.]]
[[File:Aircraft flaps.svg|thumb|right|[[flap (aircraft)|Flaps]] (green) are used in various configurations to increase the wing area and to increase the lift. In conjunction with [[spoiler (aeronautics)|spoilers]] (red), flaps maximize drag and minimize lift during the landing roll.]]
{{Main|Lift (force)}}
{{Main|Lift (force)}}
The design and analysis of the wings of aircraft is one of the principal applications of the science of [[aerodynamics]], which is a branch of [[fluid mechanics]]. In principle, the properties of the airflow around any moving object can be found by solving the [[Navier-Stokes equations]] of [[fluid dynamics]]. However, except for simple geometries these equations are notoriously difficult to solve and simpler equations are used.<ref name=Nasa_NS>{{cite web |url=http://www.grc.nasa.gov/WWW/K-12/airplane/nseqs.html |title=Navier-Stokes Equations |publisher=[[Glenn Research Center]] |date=2012-04-16 |access-date=2012-04-25}}</ref>
The design and analysis of the wings of aircraft is one of the principal applications of the science of [[aerodynamics]], which is a branch of [[fluid mechanics]]. In principle, the properties of the airflow around any moving object can be found by solving the [[Navier-Stokes equations]] of [[fluid dynamics]]. However, except for simple geometries, these equations are notoriously difficult to solve and simpler equations are used.<ref name=Nasa_NS>{{cite web |url=http://www.grc.nasa.gov/WWW/K-12/airplane/nseqs.html |title=Navier-Stokes Equations |publisher=[[Glenn Research Center]] |date=2012-04-16 |access-date=2012-04-25}}</ref>


For a wing to produce ''lift'', it must be oriented at a suitable [[angle of attack]]. When this occurs, the wing deflects the airflow downwards as it passes the wing. Since the wing exerts a force on the air to change its direction, the air must also exert an equal and opposite force on the wing.<ref name=HR_378a>{{cite book |quote=...the effect of the wing is to give the air stream a downward velocity component. The reaction force of the deflected air mass must then act on the wing to give it an equal and opposite upward component. |first1=David |last1=Halliday |first2=Robert |last2=Resnick |title=Fundamentals of Physics |edition=3rd |publisher=[[John Wiley & Sons]] |page=378}}</ref><ref>"If the body is shaped, moved, or inclined in such a way as to produce a net deflection or turning of the flow, the local velocity is changed in magnitude, direction, or both. Changing the velocity creates a net force on the body" {{cite web |publisher=[[Glenn Research Center]] |title=Lift from Flow Turning |url=http://www.grc.nasa.gov/WWW/K-12/airplane/right2.html |access-date=2011-06-29}}</ref><ref name="Weltner_Physics_of_Flight_Reviewed">"The cause of the aerodynamic lifting force is the downward acceleration of air by the airfoil..." {{cite web |last1=Weltner |first1=Klaus |last2=Ingelman-Sundberg |first2=Martin |title=Physics of Flight – reviewed |website=[[Goethe University Frankfurt]] |url=http://user.uni-frankfurt.de/~weltner/Flight/PHYSIC4.htm |url-status=dead |archive-url=https://web.archive.org/web/20110719102847/http://user.uni-frankfurt.de/~weltner/Flight/PHYSIC4.htm |archive-date=2011-07-19}}</ref><ref>{{cite web |url=https://www.grc.nasa.gov/WWW/k-12/VirtualAero/BottleRocket/airplane/wrong1.html |title=Incorrect Lift Theory |website=[[Glenn Research Center]]}}</ref> <!-- Uncited.
For a wing to produce ''lift'', it must be oriented at a suitable [[angle of attack]]. When that occurs, the wing deflects the airflow downwards as it passes the wing. Since the wing exerts a force on the air to change its direction, the air must also exert an equal and opposite force on the wing.<ref name=HR_378a>{{cite book |quote=...the effect of the wing is to give the air stream a downward velocity component. The reaction force of the deflected air mass must then act on the wing to give it an equal and opposite upward component. |first1=David |last1=Halliday |first2=Robert |last2=Resnick |title=Fundamentals of Physics |edition=3rd |publisher=[[John Wiley & Sons]] |page=378}}</ref><ref>"If the body is shaped, moved, or inclined in such a way as to produce a net deflection or turning of the flow, the local velocity is changed in magnitude, direction, or both. Changing the velocity creates a net force on the body" {{cite web |publisher=[[Glenn Research Center]] |title=Lift from Flow Turning |url=http://www.grc.nasa.gov/WWW/K-12/airplane/right2.html |access-date=2011-06-29}}</ref><ref name="Weltner_Physics_of_Flight_Reviewed">"The cause of the aerodynamic lifting force is the downward acceleration of air by the airfoil..." {{cite web |last1=Weltner |first1=Klaus |last2=Ingelman-Sundberg |first2=Martin |title=Physics of Flight – reviewed |website=[[Goethe University Frankfurt]] |url=http://user.uni-frankfurt.de/~weltner/Flight/PHYSIC4.htm |url-status=dead |archive-url=https://web.archive.org/web/20110719102847/http://user.uni-frankfurt.de/~weltner/Flight/PHYSIC4.htm |archive-date=2011-07-19}}</ref><ref>{{cite web |url=https://www.grc.nasa.gov/WWW/k-12/VirtualAero/BottleRocket/airplane/wrong1.html |title=Incorrect Lift Theory |website=[[Glenn Research Center]]}}</ref> <!-- Uncited.


A region of lower-than-normal air pressure is generated over the top surface of the wing, with a higher pressure on the bottom of the wing. These air pressure differences can be measured directly using instrumentation or can be calculated from the airspeed distribution using basic [[physics|physical principles]] such as [[Bernoulli's principle]], which relates changes in air speed to changes in air pressure.
A region of lower-than-normal air pressure is generated over the top surface of the wing, with a higher pressure on the bottom of the wing. These air pressure differences can be measured directly using instrumentation or can be calculated from the airspeed distribution using basic [[physics|physical principles]] such as [[Bernoulli's principle]], which relates changes in air speed to changes in air pressure.
Line 31: Line 31:
== Design features ==
== Design features ==
{{main|Wing configuration}}
{{main|Wing configuration}}
[[File:bmi a319-100 g-dbca closeup arp.jpg|thumb|right|The wing of a landing [[BMI (airline)|BMI]] [[Airbus]] [[A319-100]]. The [[leading edge slats|slats]] at its [[leading edge]] and the [[flap (aircraft)|flap]]s at its [[trailing edge]] are extended.]]
[[File:bmi a319-100 g-dbca closeup arp.jpg|thumb|right|The wing of a landing [[BMI (airline)|BMI]] [[Airbus]] [[A319-100]]; the [[leading edge slats|slats]] at its [[leading edge]] and the [[flap (aircraft)|flap]]s at its [[trailing edge]] are extended]]
Aircraft wings may feature some of the following:
Aircraft wings may feature some of the following:
* A rounded [[leading edge]] cross-section
* A rounded [[leading edge]] cross-section
Line 70: Line 70:
{{further|Bird's wing}}
{{further|Bird's wing}}
{{further|Insect wing}}
{{further|Insect wing}}
In nature, wings have [[evolution|evolved]] in [[insect]]s, [[pterosaur]]s, [[dinosaurs]] ([[bird]]s, [[Scansoriopterygidae]]), and mammals ([[bat]]s) as a means of [[Animal locomotion|locomotion]]. Various species of [[penguin]]s and other flighted or [[flightless bird|flightless]] water birds such as [[auk]]s, [[cormorant]]s, [[guillemot]]s, [[shearwater]]s, [[eider duck|eider]] and scoter ducks and diving [[petrel]]s are avid swimmers, and use their wings to propel through water.<ref>{{cite web |url=http://www.stanford.edu/group/stanfordbirds/text/essays/Swimming.html |title=Swimming |publisher=[[Stanford university]] |access-date=2012-04-25}}</ref>
In nature, wings have [[evolution|evolved]] in [[insect]]s, [[pterosaur]]s, [[dinosaurs]] ([[bird]]s, [[Scansoriopterygidae]]), and mammals ([[bat]]s) as a means of [[Animal locomotion|locomotion]]. Various species of [[penguin]]s and other flighted or [[flightless bird|flightless]] water birds such as [[auk]]s, [[cormorant]]s, [[guillemot]]s, [[shearwater]]s, [[eider duck|eider]] and scoter ducks, and diving [[petrel]]s are avid swimmers using their wings to propel themselves through water.<ref>{{cite web |url=http://www.stanford.edu/group/stanfordbirds/text/essays/Swimming.html |title=Swimming |publisher=[[Stanford university]] |access-date=2012-04-25}}</ref>
<div class="center">
<div class="center">
;Wing forms in nature
;Wing forms in nature
Line 82: Line 82:


===Tensile structures===
===Tensile structures===
In 1948, [[Francis Rogallo]] invented a kite-like [[Rogallo wing|tensile wing]] supported by inflated or rigid struts, which ushered in new possibilities for aircraft.<ref>{{cite web |url=https://history.nasa.gov/SP-4308/ch11.htm#382 |title=Rogallo Wing -the story told by NASA |website=History.nasa.gov |access-date=2012-12-23}}</ref> Near in time, [[Domina Jalbert]] invented flexible un-sparred ram-air airfoiled thick wings. These two new branches of wings have been since extensively studied and applied in new branches of aircraft, especially altering the personal recreational aviation landscape.<ref>{{Cite book |url=https://archive.org/details/goldenknightsusa0000hopk |url-access=registration |quote=Domina Jalbert ram air wing. |title=The Golden Knights: The U.S. Army Parachute Team |last1=Hopkins |first1=Ellen |last2=Bledsoe |first2=Glen |date=2001 |publisher=Capstone |isbn=9780736807753 |pages=[https://archive.org/details/goldenknightsusa0000hopk/page/21 21] |language=en}}</ref>
In 1948, [[Francis Rogallo]] invented a kite-like [[Rogallo wing|tensile wing]] supported by inflated or rigid struts, which ushered in new possibilities for aircraft.<ref>{{cite web |url=https://history.nasa.gov/SP-4308/ch11.htm#382 |title=Rogallo Wing -the story told by NASA |website=History.nasa.gov |access-date=2012-12-23}}</ref> Near that time, [[Domina Jalbert]] invented flexible un-sparred ram-air airfoiled thick wings. These two new branches of wings have been since extensively studied and applied in new branches of aircraft, especially altering the personal recreational aviation landscape.<ref>{{Cite book |url=https://archive.org/details/goldenknightsusa0000hopk |url-access=registration |quote=Domina Jalbert ram air wing. |title=The Golden Knights: The U.S. Army Parachute Team |last1=Hopkins |first1=Ellen |last2=Bledsoe |first2=Glen |date=2001 |publisher=Capstone |isbn=9780736807753 |pages=[https://archive.org/details/goldenknightsusa0000hopk/page/21 21] |language=en}}</ref>


== See also ==
== See also ==

Revision as of 01:14, 25 June 2024

Wing of a Eurasian magpie, which allows flight by the flapping of wings
A swept wing KC-10 Extender (top) refuels a trapezoidal-wing F-22 Raptor

A wing is a type of fin which produces lift while moving through air or some other fluid. Accordingly, wings have streamlined cross-sections which are subject to aerodynamic forces and act as airfoils. A wing's aerodynamic efficiency is expressed as its lift-to-drag ratio. The lift a wing generates at a given speed and angle of attack can be one to two orders of magnitude greater than the total drag on the wing. A high lift-to-drag ratio requires a significantly smaller thrust to propel the wings through the air at sufficient lift.

Lifting structures used in water include various foils like hydrofoils. Hydrodynamics is the governing science, rather than aerodynamics. Applications of underwater foils occur in hydroplanes, sailboats, and submarines.

Etymology and usage

For many centuries, the word "wing", from the Old Norse vængr,[1] referred mainly to the foremost limbs of birds (in addition to the architectural aisle). But in recent centuries the word's meaning has extended to include lift producing appendages of insects, bats, pterosaurs, boomerangs, some sail boats, and aircraft or the inverted airfoil on a race car which generates a downward force to increase traction.

Aerodynamics

Condensation in the low pressure region over the wing of an Airbus A340, passing through humid air
Flaps (green) are used in various configurations to increase the wing area and to increase the lift. In conjunction with spoilers (red), flaps maximize drag and minimize lift during the landing roll.

The design and analysis of the wings of aircraft is one of the principal applications of the science of aerodynamics, which is a branch of fluid mechanics. In principle, the properties of the airflow around any moving object can be found by solving the Navier-Stokes equations of fluid dynamics. However, except for simple geometries, these equations are notoriously difficult to solve and simpler equations are used.[2]

For a wing to produce lift, it must be oriented at a suitable angle of attack. When that occurs, the wing deflects the airflow downwards as it passes the wing. Since the wing exerts a force on the air to change its direction, the air must also exert an equal and opposite force on the wing.[3][4][5][6]

Cross-sectional shape

An airfoil (American English) or aerofoil (British English) is the shape of a wing, blade (of a propeller, rotor, or turbine), or sail (as seen in cross-section). Wings with an asymmetrical cross section are the norm in subsonic flight. Wings with a symmetrical cross section can also generate lift by using a positive angle of attack to deflect air downward. Symmetrical airfoils have higher stalling speeds than cambered airfoils of the same wing area[7] but are used in aerobatic aircraft[8] as they provide practical performance whether the aircraft is upright or inverted. Another example comes from sailboats, where the sail is a thin membrane with no path-length difference between one side and the other.[9]

For flight speeds near the speed of sound (transonic flight), airfoils with complex asymmetrical shapes are used to minimize the drastic increase in drag associated with airflow near the speed of sound.[10] Such airfoils, called supercritical airfoils, are flat on top and curved on the bottom.[11]

Design features

The wing of a landing BMI Airbus A319-100; the slats at its leading edge and the flaps at its trailing edge are extended

Aircraft wings may feature some of the following:

  • A rounded leading edge cross-section
  • A sharp trailing edge cross-section
  • Leading-edge devices such as slats, slots, or extensions
  • Trailing-edge devices such as flaps or flaperons (combination of flaps and ailerons)
  • Winglets to keep wingtip vortices from increasing drag and decreasing lift
  • Dihedral, or a positive wing angle to the horizontal, increases spiral stability around the roll axis, whereas anhedral, or a negative wing angle to the horizontal, decreases spiral stability.

Aircraft wings may have various devices, such as flaps or slats that the pilot uses to modify the shape and surface area of the wing to change its operating characteristics in flight.

Wings may have other minor independent surfaces.

Applications and variants

Besides fixed-wing aircraft, applications for wing shapes include:

In nature

In nature, wings have evolved in insects, pterosaurs, dinosaurs (birds, Scansoriopterygidae), and mammals (bats) as a means of locomotion. Various species of penguins and other flighted or flightless water birds such as auks, cormorants, guillemots, shearwaters, eider and scoter ducks, and diving petrels are avid swimmers using their wings to propel themselves through water.[17]

Wing forms in nature

Tensile structures

In 1948, Francis Rogallo invented a kite-like tensile wing supported by inflated or rigid struts, which ushered in new possibilities for aircraft.[18] Near that time, Domina Jalbert invented flexible un-sparred ram-air airfoiled thick wings. These two new branches of wings have been since extensively studied and applied in new branches of aircraft, especially altering the personal recreational aviation landscape.[19]

See also

Natural world
Aviation
Sailing

References

  1. ^ "Online Etymology Dictionary". Etymonline.com. Retrieved 2012-04-25.
  2. ^ "Navier-Stokes Equations". Glenn Research Center. 2012-04-16. Retrieved 2012-04-25.
  3. ^ Halliday, David; Resnick, Robert. Fundamentals of Physics (3rd ed.). John Wiley & Sons. p. 378. ...the effect of the wing is to give the air stream a downward velocity component. The reaction force of the deflected air mass must then act on the wing to give it an equal and opposite upward component.
  4. ^ "If the body is shaped, moved, or inclined in such a way as to produce a net deflection or turning of the flow, the local velocity is changed in magnitude, direction, or both. Changing the velocity creates a net force on the body" "Lift from Flow Turning". Glenn Research Center. Retrieved 2011-06-29.
  5. ^ "The cause of the aerodynamic lifting force is the downward acceleration of air by the airfoil..." Weltner, Klaus; Ingelman-Sundberg, Martin. "Physics of Flight – reviewed". Goethe University Frankfurt. Archived from the original on 2011-07-19.
  6. ^ "Incorrect Lift Theory". Glenn Research Center.
  7. ^ Laitone, E. V. (1997). "Wind tunnel tests of wings at Reynolds numbers below 70 000". Experiments in Fluids. 23 (405): 405–409. doi:10.1007/s003480050128. S2CID 122755021.
  8. ^ "What are acrobatic and aerobatic flight?". Federal Aviation Administration. Retrieved 26 October 2022.
  9. ^ "...consider a sail that is nothing but a vertical wing (generating side-force to propel a yacht). ...it is obvious that the distance between the stagnation point and the trailing edge is more or less the same on both sides. This becomes exactly true in the absence of a mast—and clearly the presence of the mast is of no consequence in the generation of lift. Thus, the generation of lift does not require different distances around the upper and lower surfaces." Holger Babinsky How do Wings Work? Physics Education November 2003, PDF
  10. ^ John D. Anderson, Jr. Introduction to Flight 4th ed page 271.
  11. ^ "Supercritical wings have a flat-on-top "upside down" look". NASA Dryden Flight Research Center.
  12. ^ Hahne, David E.; Jordan, Frank L. Jr. (1991). Semi-span full-scale tests of a business-jet wing with a natural laminar flow airfoil. National Aeronautics and Space Administration, Scientific and Technical Information Office. p. 5 – via Google Books.
  13. ^ "The Physics Of Kite Flying – Aerodynamic Lift". RealWorldPhysicsProblems.com. real-world-physics-problems.com. Retrieved 28 January 2022.
  14. ^ López, Harm Frederik Althuisius. "Helicopter physics" (PDF). ColoradoCollege.edu. Colorado College Dept. of Physics. Retrieved 28 January 2022.
  15. ^ "Rocket aerodynamics". Sciencelearn.org.nz. New Zealand Government Ministry of Business, Innovation & Employment. Retrieved 28 January 2022.
  16. ^ Zoechling, Moritz (20 January 2015). "Aerodynamics on Formula 1 Race Cars". APlusPhysics.com. A Plus Physics. Retrieved 28 January 2022.
  17. ^ "Swimming". Stanford university. Retrieved 2012-04-25.
  18. ^ "Rogallo Wing -the story told by NASA". History.nasa.gov. Retrieved 2012-12-23.
  19. ^ Hopkins, Ellen; Bledsoe, Glen (2001). The Golden Knights: The U.S. Army Parachute Team. Capstone. pp. 21. ISBN 9780736807753. Domina Jalbert ram air wing.