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NASA/LANGLEY RC-SC2 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILENASA/LANGLEY RC-SC2 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 39%c
max camber0.6% @ 63%c
LE radius1.09%c
area upper / chord0.0416
area lower / chord-0.0328
area camber / chord0.0044
TE thickness0.21%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7298-50.17083.3331.07111.671.97220ClAngle 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 0.02849% of chord; maximum error 0.1529%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
131
Angle at maximum lift / drag (°)
11
Minimum Cd
0.006933
Maximum Cl
1.747
Angle at maximum Cl (°)
17
Cd at zero lift
0.006935
Cm at zero angle
-0.02097
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…