UIUC Airfoil Coordinates Database. Master of typing in chinese 3 2 2013. Included below are coordinates for nearly 1,600 airfoils (Version 2.0). The UIUC Airfoil Data Site gives some background on the database. The hot-wire sensor was positioned between 0.5 mm and 0.7 mm above the airfoil surface. This offset distance was regularly checked and its effects are accounted in velocity profile data. In general, the profile measurements were acquired close enough to capture the reattachment location with accuracy of 2.5% of chord.
Airfoil 5 8 7 Mm Equals
| wing span | 3190 mm |
| length | 1507 mm |
| weight | 2200 g |
| wing airfoil | HN-483 |
| wing area | 64 dm2 |
| elevator airfoil | HN-470S |
| elevator area | 6,1 dm2 |
Airfoil 5 8 7 Mm Socket
| Settings FURIO V | |||||
| seting | CG | FLAPS | AILERONS | ELEVATOR | RUDDER |
| A | 106 | - 4 | - 2 | + 1 | 0 |
| B | 106 | 0 | 0 | 0 | 0 |
| C | 106 | + 2 | + 2 | 0 | 0 |
| START | - 16 | - 13 | + 1 | 0 | |
| BUTTERFLY | - 50 | + 15 | - 6 | 0 | |
| deflections | CG | FLAPS | AILERONS | ELEVATOR | RUDDER |
| A | 106 | - 6 / + 15 | + 11 / - 7 | + 13 / - 8 | |
| B | 106 | - 5 / + 8 | - 6 / + 10 | + 11 / - 7 | + 13 / - 8 |
| C | 106 | - 8 / + 6 | - 7 / + 9 | + 9 / - 6 | 0 |
| START | - 7 / +10 | +10 / -8 | + 10 / - 6 | ||
| wing mix | CG | FLAPS | AILERONS | ELEVATOR | RUDDER |
| A | ELEVATOR > FLAPS & AILERONS | 106 | |||
| A | AILERONS > RUDDER | 106 | - 6 / + 15 | - 3 / + 5 | |
| B | ELEVATOR > FLAPS & AILERONS | 106 | - 5 | - 3 | + 11 |
| C | ELEVATOR > FLAPS & AILERONS | 106 | - 3 | - 1 | + 9 |
| S | AILERONS > RUDDER | - 7 / + 10 | - 3 / + 5 | ||
| Flap down = - , Flap up = + , all is in mm. |
