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DargPolarAL.png (573 × 305 pixels, file size: 11 KB, MIME type: image/png)
Summary
Summary
| Description |
English: Plot of the drag polar CD = 0.017 + 0.075.(CL - 0.1)^2, parameter values typical of small aircraft. tangent is to point of maximum L/D |
|---|---|
| Source |
Own work |
| Date |
2012-06-08 |
| Author | |
| Permission (Reusing this file) |
See below.
|
Licensing
I, the copyright holder of this work, hereby publish it under the following license:
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Licensing
I, the copyright holder of this work, hereby publish it under the following license:
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 17:27, 20 November 2023 | | 573 × 305 (11 KB) | Isidore (talk | contribs) | =={{int:filedesc}}== {{Information |description={{en|1=Plot of the drag polar CD = 0.017 + 0.075.(CL - 0.1)^2, parameter values typical of small aircraft. tangent is to point of maximum L/D}} |date=2012-06-08 |source={{own}} |author=TSRL |permission= |other_versions= |other_fields= }} =={{int:license-header}}== {{self|cc-by-sa-3.0}} Category:Aerodynamics diagrams Category:Lift and drag curves =={{int:license-header}}== {{self|cc-by-sa-3.0}} [[Category:Aerodynamics... |
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