File:Subsonic and trans-sonic airfoils.svg
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DescriptionSubsonic and trans-sonic airfoils.svg |
English: Subsonic (1) and trans-sonic (2) airfoils at identical Mach number.
A: Supersonic flow region B: Shock wave C: Area of stalled flow On the trans-sonic (or supercritical) airfoil, the deceleration of the flow on the top surface, and the strength of the shockwave with which the flow returns to a subsonic regime, are reduced. As a consequence, the stalled flow region, which occurs much further down the airfoil, is much smaller. Supercritical airfoils are used on all modern civilian airliners.Français : Profils subsonique (1) et trans-sonique (2) observés à la même vitesse.
A: Zone d’écoulement supersonique B: Onde de choc C: Zone d’écoulement séparé turbulent La décélération de l’air sur l’extrados, ainsi que la puissance de l’onde de choc qui caractérise son retour à un régime subsonique, sont réduits sur le profil trans-sonique (ou "supercritique"). La zone d’écoulement séparé turbulent, qui débute plus loin sur le profil, est en conséquence réduite. Les profils trans-soniques sont utilisés sur tous les avions de ligne modernes. |
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Date | |||
Source | Own work based on: Airfoils.svg by Pbroks13 | ||
Author | Olivier Cleynen | ||
SVG development InfoField | This diagram was created with Inkscape.
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This image is a derivative work of the following images:
- File:Airfoils.svg licensed with PD-USGov-NASA
- 2008-06-07T04:02:12Z File Upload Bot (Magnus Manske) 182x199 (13392 Bytes) {{BotMoveToCommons|en.wikipedia}} {{Information |Description={{en|SVG redraw of [[:en::Image:Airfoils.jpg]]}} |Source=Transferred from [http://en.wikipedia.org en.wikipedia]; transfered to Commons by [[User:Pbroks13]] using
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 12:38, 13 August 2011 | 1,297 × 1,954 (19 KB) | Ariadacapo (talk | contribs) | {{Information |Description= {{en|Subsonic ('''1''') and trans-sonic ('''2''') airfoils at identical Mach number. '''A''': Supersonic flow region '''B''': Shock wave '''C''': Area of stalled flow On the trans-sonic (or supercritical) airfoil, the decel |
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