File:Polar diagram of coefficients of lift and drag for angles of attack.png
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Polar_diagram_of_coefficients_of_lift_and_drag_for_angles_of_attack.png (720 × 540 pixels, file size: 66 KB, MIME type: image/png)
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
I, the copyright holder of this work, hereby publish it under the following license:
This file is licensed under the Creative Commons Attribution-Share Alike 4.0 International license.
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- to share – to copy, distribute and transmit the work
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- attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 18:32, 6 April 2015 | | 720 × 540 (66 KB) | wikimediacommons>HopsonRoad | Show flow status. |
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