LIFT CL 0.00
DRAG CD 0.00
L/D —
FLOW —
NACA 0012 · α 6.0°
Re 0
fps 0
Test body
Config
Target α
Wind speed
AOA TRANSITION
α live 6.0°
Viscosity
like: air
Fluid preset
Render
Smoke density
Quality
Export
Lift curve — CL vs α
● CL ● CD ○ live
Time history — forces
● CL ● CD
Pressure — −Cp vs x/c
● upper ● lower