File:DargPolarAL.png
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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 |
| Date | |
| Source | Own work |
| Author | TSRL |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 20:21, 8 June 2012 | | 573 × 305 (11 KB) | TSRL |
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