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NASA/LANGLEY RC12-64C AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILENASA/LANGLEY RC12-64C AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 40%c
max camber1.0% @ 35%c
LE radius1.59%c
area upper / chord0.0497
area lower / chord-0.0370
area camber / chord0.0063
TE thickness0.24%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6832-50.15573.3330.994711.671.83420ClAngle 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 0.02919% of chord; maximum error 0.1379%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
122.7
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007312
Maximum Cl
1.624
Angle at maximum Cl (°)
16
Cd at zero lift
0.007318
Cm at zero angle
-0.01655
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…