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CAMBEREDRESEARCHSELIG-DATABASE

RAF 32MD

Cambered · 10% thick · low-to-mid Re
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PROFILERAF 32MD
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.2% @ 30%c
max camber4.0% @ 50%c
LE radius1.14%c
area upper / chord0.0605
area lower / chord-0.0072
area camber / chord0.0266
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1948-50.37453.3330.943811.671.51320ClAngle 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 0.05886% of chord; maximum error 0.2416%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
151.3
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006288
Maximum Cl
1.371
Angle at maximum Cl (°)
7
Cd at zero lift
0.006345
Cm at zero angle
-0.1351
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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