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CAMBEREDS/SC SERIESSELIG-DATABASE

NASA SC(2)-0714 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILENASA SC(2)-0714 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.0% @ 37%c
max camber1.5% @ 80%c
LE radius2.15%c
area upper / chord0.0508
area lower / chord-0.0429
area camber / chord0.0039
TE thickness0.70%c
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Polars

Preliminary
NeuralFoil
-0.2569-50.61083.3331.47811.672.34620ClAngle 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 0.01378% of chord; maximum error 0.04779%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
140.1
Angle at maximum lift / drag (°)
9
Minimum Cd
0.008189
Maximum Cl
2.129
Angle at maximum Cl (°)
15
Cd at zero lift
0.008207
Cm at zero angle
-0.1439
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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