File:Vought F-8 Crusader Supercritical Wing 3-view line art (EG-0029-01).gif

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Description	English: The F-8 Supercritical Wing was a flight research project designed to test a new wing concept designed by Dr. Richard Whitcomb, chief of the Transonic Aerodynamics Branch, Langley Research Center, Hampton, Virginia. Compared to a conventional wing, the supercritical wing (SCW) is flatter on the top and rounder on the bottom with a downward curve at the trailing edge. The Supercritical Wing was designed to delay the formation of and reduce the shock wave over the wing just below and above the speed of sound (transonic region of flight). Delaying the shock wave at these speeds results in less drag.
Date	Taken in February 1998
Source	https://www.dfrc.nasa.gov/Gallery/Graphics/F-8SCW/index.html (image link)
Author	NASA/DFRC

This image or video was catalogued by Armstrong Flight Research Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: EG-0029-01.

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	Date/Time	Thumbnail	Dimensions	User	Comment
current	06:09, 9 October 2021		3,030 × 2,606 (106 KB)	Huntster (talk \| contribs)	== {{int:filedesc}} == {{Information \|Description={{en\|1=The F-8 Supercritical Wing was a flight research project designed to test a new wing concept designed by Dr. Richard Whitcomb, chief of the Transonic Aerodynamics Branch, Langley Research Center, Hampton, Virginia. Compared to a conventional wing, the supercritical wing (SCW) is flatter on the top and rounder on the bottom with a downward curve at the trailing edge. The Supercritical Wing was designed to delay the formation of and redu...

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