aircraft:tmd:airfoil
Differences
This shows you the differences between two versions of the page.
| Both sides previous revisionPrevious revision | Next revisionBoth sides next revision | ||
| aircraft:tmd:airfoil [2017/03/02 11:15] – [Table of flap coefficients] jh | aircraft:tmd:airfoil [2017/03/02 11:19] – [Table of flap coefficients] jh | ||
|---|---|---|---|
| Line 118: | Line 118: | ||
| | Fowler flap | 1.4 ... 3.0 | 0.14 ... 0.3 | -0.73 | | | Fowler flap | 1.4 ... 3.0 | 0.14 ... 0.3 | -0.73 | | ||
| + | Recommended values for the Aerofly are: | ||
| + | |||
| + | ^ Type of flap ^ ClFlap | ||
| + | | Plain flap | 2.1 | 0.0 | -0.2 ... -0.5 | | ||
| + | | Split flap | 2.4 | 0.2 | -0.2 ... -0.9 | | ||
| + | | Slotted flap | 2.7 | 0.06 | -0.2 | | ||
| + | | Fowler flap | 2.7 ... 3.4 | 0.2 | -0.6 ... -1.1 | | ||
| ==== ClAlphaBase ==== | ==== ClAlphaBase ==== | ||
aircraft/tmd/airfoil.txt · Last modified: 2020/09/28 22:44 by jh