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DELFT DU84-132V3 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILEDELFT DU84-132V3 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.6% @ 34%c
max camber3.1% @ 45%c
LE radius2.05%c
area upper / chord0.0681
area lower / chord-0.0224
area camber / chord0.0229
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.2527-50.34413.3330.940911.671.53820ClAngle of attack (°)
Why this curve

This is a NeuralFoil prediction from the stored profile coordinates and the selected flow condition, with AeroSandbox compressibility corrections. It is not a completed OpenFOAM calculation.

Prediction error has not been calibrated for this condition. No accuracy interval is claimed.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.02808% of chord; maximum error 0.08827%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
146.7
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006691
Maximum Cl
1.388
Angle at maximum Cl (°)
8
Cd at zero lift
0.006702
Cm at zero angle
-0.1198
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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