Kutta Condition &
Lift
un
seel
.com · circulation · trailing edge · L' = ρVΓ
angle of attack
0°
circulation Γ
0 m²/s
lift L'
0 N/m
state
standby
airfoil (wing)
fast flow over top
slow flow underneath
starting / bound vortex
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.com · Kutta Condition & Lift