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RAF 30MD

Symmetric · 8% thick · low-to-mid Re
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PROFILERAF 30MD
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.6% @ 30%c
max camber0.0% @ 0%c
LE radius0.64%c
area upper / chord0.0252
area lower / chord-0.0252
area camber / chord0.0000
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7632-50.060313.3330.883811.671.70720ClAngle 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 0.04197% of chord; maximum error 0.2042%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
97.56
Angle at maximum lift / drag (°)
9
Minimum Cd
0.007126
Maximum Cl
1.501
Angle at maximum Cl (°)
16
Cd at zero lift
0.007126
Cm at zero angle
2.259e-16
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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