Je kan alleszins wat dingen aanpassen in de .par file van het betreffende model.
Even zoeken wat je precies weer kan veranderen.
Edit: dit is wat ik erover kon vinden. Lijkt me dus dat je de waarde op de 2de regel van de .par file stapsgewijs kan verhogen, naar jouw wensen.
1: Type: 0=plane, 1=heli
2: Tmax: max thrust in newtons, if you increase this the plane seems to fly faster, as you'd expect.
3: Drmax: max rudder angle in radians
4: Demax: max elevator angle in radians
5: Damax: max aileron angle in radians
All three work well to adjust the sensitivity of the model flying to the affects of the control throws. I've used these to calm down a twitchy model to act more sedate.
6: CLmax: max lift coefficient
7: CLmin: min lift coefficient
8: CLa: Lift Gradient, per radian
9: CLast: Lift Gradient in a stall, per radian
These numbers seem like multipliers to the lift coefficient but I can't be sure. Messing with them can make your model accelerate to amazing speeds. Anyone had success understanding them?
10: CDw: Drag Coefficient of Wing
11: CDb: Drag Coefficient of Fuse
12: mug: friction coefficient of the wheels
13: dCDSt: rise of drag coefficient in a stall
All are very low numbers and don't seem to have a large affect but may be related as lift to drag ratios. Any insights?
14: CM: Moment Coefficient
Someone else translated this as the stall poiint of the main wing. It's usually a small negative number with no obvious dependencies.
15: alpha0: wing angle in radians
16: b: wing span in meters
17: c: wing chord in meters
All seem obvious but not sure how they affect model actions.
18: hce: equivalent center of gravity, from leading edge in meters
Moving the CG works like in an actual model plane.
19: m: mass of model in kilograms
Adding mass makes the model more sluggish, removing it makes it more agile.
The next three items mention inertia moments. I've not a clue what they're supposed to do except maybe the affects of airframe acceleration in one direction or another around the 3 flight axis.
20: lzz: Yaw Inertia Coefficient Kg*m^2
21: Iyy: Pitch Inertia Coefficient Kg*m^2
22: Ixx: Roll Inertia Coefficient Kg*m^2
23: Effective horiz. stab area m^2
24: Effective vert. stab area m^2
Both should increase control surface response as increased.
25: Lt: Tail moment arm in meters
Should decrease the effect of stabilizer controls when shorter and increase effect when longer.
26: VForm: Effect of Dihedral Angle
This acts as a self righting quality of high dihedral and polyhedral wings. As you'd expect the numbers are higher for the Tipsy and SilkyWind400 models.
