File:Subsonic and trans-sonic airfoils.svg

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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.
Date
Source Own work based on: Airfoils.svg by Pbroks13
Author Olivier Cleynen
SVG development
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This diagram was created with Inkscape.
 
This diagram uses embedded text/digits.
This diagram is a retouched picture, which means that it has been digitally altered from its original version. Modifications: Changed supercritical airfoil angle of attack, redrew supersonic zones, removed text to make i18n easier, increased size. Everything re-drawn.. The original can be viewed here: Airfoils.svg. Modifications made by Ariadacapo.

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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/TimeThumbnailDimensionsUserComment
current12:38, 13 August 2011Thumbnail for version as of 12:38, 13 August 20111,297 × 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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