File:Polar diagram of coefficients of lift and drag for angles of attack.png
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Summary
| Description |
English: Polar diagram of coefficients of lift (CL) and drag (CD) for the angles of attack shown for a hypothetical sail. The dotted line is tangential with the point of highest ratio of lift over drag (CL / CD). Also shown is flow status, ranging from attached to stalled. |
| Date | |
| Source | Own work |
| Author | HopsonRoad |
Licensing
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File history
Click on a date/time to view the file as it appeared at that time.
| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 17:32, 6 April 2015 | | 720 × 540 (66 KB) | HopsonRoad | Show flow status. |
| 21:18, 4 April 2015 |  | 720 × 540 (57 KB) | HopsonRoad | Axes, tick marks | |
| 18:15, 4 April 2015 |  | 720 × 540 (54 KB) | HopsonRoad | User created page with UploadWizard |
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