File:Supercrit.jpg
Supercrit.jpg (451 × 323 pixels, file size: 11 KB, MIME type: image/jpeg)
Summary[edit]
| Description |
Supercritical airfoil Mach Number/pressure coefficient diagram. The sudden increase in pressure coefficient at midchord is due to the shock. (y-axis:Mach number (or pressure coefficient, negative up); x-axis: position along chord, leading edge left) |
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| Source |
Own work ; Diagram/chart prepared by uploader. |
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| Permission (Reusing this file) |
See below.
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Licensing[edit]
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 16:09, 3 November 2005 | | 451 × 323 (11 KB) | Fongs (talk | contribs) | author: philip poppe |
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