Narzędzia
Kąt natarcia i decalage
Wizualizacja czysto geometryczna, bez symulacji aerodynamiki. Każda zmiana wymaga bezpiecznego próbnego ślizgu.
Wing incidence2.0°
Stabilizer incidence0.0°
Decalage (wing − stab): 2°
ƒdecalage = α_wing − α_stab
Side view
Result
Decalage (wing − stab): 2°
Possible effect: Flat glide, neutral characteristics; typical starting range.
Decalage is the difference between wing and stabilizer incidence. More positive decalage typically increases climb and stall tendency; less gives a flatter glide or dive tendency. These relationships are indicative only; always verify with safe test glides.
⚠Sliders illustrate geometry only; they do not simulate aerodynamics. Each change requires a safe test glide.