Test object
NACA 2412 airfoil
Sports car
Reference sphere
Wind speed
32 m/s
Angle of attack
6°
Smoke density
70%
Dynamic pressure
627 Pa
Lift
2.84 kN
Drag
0.29 kN
RUNNING · STEADY FLOW
Re 4.38 × 10⁶
FLOW
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HIGH PRESSURE
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