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CAMBEREDRESEARCHSELIG-DATABASE

OAF102 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEOAF102 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.2% @ 28%c
max camber3.6% @ 53%c
LE radius1.14%c
area upper / chord0.0541
area lower / chord-0.0093
area camber / chord0.0224
TE thickness1.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3454-50.53543.3331.41611.672.29720ClAngle 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.

Geometry fit: RMS error 0.00531% of chord; maximum error 0.02381%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
136.7
Angle at maximum lift / drag (°)
9
Minimum Cd
0.007693
Maximum Cl
2.077
Angle at maximum Cl (°)
16
Cd at zero lift
0.007694
Cm at zero angle
-0.1224
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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