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CAMBEREDS/SC SERIESSELIG-DATABASE

NASA SC(2)-0614 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILENASA SC(2)-0614 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.0% @ 36%c
max camber1.3% @ 80%c
LE radius2.16%c
area upper / chord0.0505
area lower / chord-0.0434
area camber / chord0.0036
TE thickness0.66%c
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Polars

Preliminary
NeuralFoil
-0.3626-50.52783.3331.41811.672.30920ClAngle 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 0.01435% of chord; maximum error 0.04824%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
139.5
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007979
Maximum Cl
2.086
Angle at maximum Cl (°)
15
Cd at zero lift
0.008002
Cm at zero angle
-0.1209
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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