Lift needed
-N
Cl
-
Drag
-N
L/D
-
Power
-W
Endurance
-min
Range
-km
Performance vs airspeed
Results
Steady level flight. Hover a row for the calculation behind it.
| Weight | -N |
|---|---|
| Lift | -N |
| Wing area used | -m^2 |
| Aspect ratio | - |
| Oswald e | - |
| Lift coefficient Cl | - |
| Induced drag Cdi | - |
| Drag coefficient Cd | - |
| Drag | -N |
| Power | -W |
| Current draw | -A |
| Run time | -min |
| Range | -m |
| Speed at target Cl | -m/s |
Vectors
Arrow length is proportional to force, scaled to fit.
Lift
Weight
Drag
Thrust