Design Studio
Shape an airfoil, set the operating point, and read the predicted flow in real time.
Airfoil
Designation
NACA 2412
%c
07
/10
07
%c
520
Operating point
°
-515
m/s
3194
Reynolds
3.23 × 10⁶
Mach
0.144
Flow field
Pressure coefficient
Streamlines
Inferring fields…
U∞ · α 4.0°
Pressure coefficient
0.000.501.00
Surface pressure
Cp along the chord, suction side up
Waiting for prediction…
Geometry
Thickness and camber distribution
Aerodynamic coefficients
Surrogate prediction with ensemble ±1σ
Cl
Cd
L/D
Cm¼
Trust & validity
Where this prediction stands
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