File:FAA-8083-3A Fig 15-9.png
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FAA-8083-3A_Fig_15-9.png (522 × 427 pixels, file size: 29 KB, MIME type: image/png)
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 07:05, 20 October 2007 | 522 × 427 (29 KB) | Mingray | {{Information |Description=High speed airplanes designed for subsonic flight are limited to some Mach number below the speed of sound to avoid the formation of shock waves that begin to develop as the airplane nears Mach 1.0. These shock waves (and the ad | |
07:05, 20 October 2007 | 522 × 427 (29 KB) | Mingray | {{Information |Description=High speed airplanes designed for subsonic flight are limited to some Mach number below the speed of sound to avoid the formation of shock waves that begin to develop as the airplane nears Mach 1.0. These shock waves (and the ad |
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