File:NASA F-8A Crusader Supercritical Wing Aircraft - GPN-2000-002001.jpg
Appearance
Size of this preview: 756 × 600 pixels. Other resolutions: 303 × 240 pixels | 605 × 480 pixels | 969 × 768 pixels | 1,280 × 1,015 pixels | 2,560 × 2,030 pixels | 3,020 × 2,395 pixels.
Original file (3,020 × 2,395 pixels, file size: 9.79 MB, MIME type: image/jpeg)
File history
Click on a date/time to view the file as it appeared at that time.
Date/Time | Thumbnail | Dimensions | User | Comment | |
---|---|---|---|---|---|
current | 20:39, 9 April 2009 | 3,020 × 2,395 (9.79 MB) | BotMultichillT | {{Information |Description={{en|1=A Vought F-8A Crusader was selected by NASA as the testbed aircraft (designated TF-8A) to install an experimental Supercritical Wing in place of the conventional wing. The unique design of the Supercritical Wing reduces t |
File usage
The following 3 pages use this file:
Global file usage
The following other wikis use this file:
- Usage on cs.wikipedia.org
- Usage on en.wikiversity.org
- Usage on it.wikipedia.org
- Usage on it.wikibooks.org
- Usage on sl.wikipedia.org