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M6 (65%)

Cambered · 8% thick · low-to-mid Re
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PROFILEM6 (65%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.8% @ 30%c
max camber1.4% @ 30%c
LE radius0.67%c
area upper / chord0.0345
area lower / chord-0.0204
area camber / chord0.0070
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7275-50.13353.3330.994511.671.85520ClAngle 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 0.02037% of chord; maximum error 0.05805%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
119.9
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006471
Maximum Cl
1.64
Angle at maximum Cl (°)
16
Cd at zero lift
0.006488
Cm at zero angle
0.002454
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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