File:Supercrit2.jpg
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Supercrit2.jpg (421 × 323 pixels, file size: 11 KB, MIME type: image/jpeg)
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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. |
Date | |
Author | |
Permission (Reusing this file) |
See below.
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Licensing
[edit]I, the copyright holder of this work, hereby release it into the public domain. This applies worldwide. If this is not legally possible: |
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File history
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 16:17, 3 November 2005 | 421 × 323 (11 KB) | Fongs (talk | contribs) | philip poppe |
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