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A63A108C

Cambered · 8% thick · low-to-mid Re
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PROFILEA63A108C
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.7% @ 30%c
max camber0.6% @ 65%c
LE radius0.66%c
area upper / chord0.0318
area lower / chord-0.0222
area camber / chord0.0048
TE thickness0.70%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.8544-50.11473.3331.08411.672.05320ClAngle 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 0.03602% of chord; maximum error 0.1106%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
129.7
Angle at maximum lift / drag (°)
11
Minimum Cd
0.006871
Maximum Cl
1.81
Angle at maximum Cl (°)
17
Cd at zero lift
0.006873
Cm at zero angle
0.002935
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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