File:PRplot.png
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Summary
| Description |
English: Plot of power required by a light aircraft of mass 000 kg, wing area 15 sq m at sea level (atmospheric density 1.2 kg/ cu m) and propeller efficiency, with drag polar drag polar CD = 0.017 + 0.075.(CL - 0.1)^2, |
| Date | |
| Source | Own work |
| Author | TSRL |
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 05:29, 11 June 2012 | | 453 × 255 (5 KB) | TSRL |
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