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CAMBEREDNACA 5-DIGITSELIG-DATABASE

NACA 65-210

Cambered · 10% thick · low-to-mid Re
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PROFILENACA 65-210
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 40%c
max camber1.1% @ 50%c
LE radius1.10%c
area upper / chord0.0405
area lower / chord-0.0245
area camber / chord0.0080
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6236-50.24733.3331.11811.671.98920ClAngle 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 0.02385% of chord; maximum error 0.1041%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
127.1
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006587
Maximum Cl
1.771
Angle at maximum Cl (°)
16
Cd at zero lift
0.006595
Cm at zero angle
-0.04309
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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