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M6 (85%)

Cambered · 10% thick · low-to-mid Re
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PROFILEM6 (85%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.2% @ 30%c
max camber1.9% @ 30%c
LE radius1.15%c
area upper / chord0.0451
area lower / chord-0.0267
area camber / chord0.0092
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7015-50.14333.3330.988111.671.83320ClAngle 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 0.02592% of chord; maximum error 0.07373%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
120.2
Angle at maximum lift / drag (°)
11
Minimum Cd
0.006891
Maximum Cl
1.622
Angle at maximum Cl (°)
17
Cd at zero lift
0.006907
Cm at zero angle
0.002135
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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