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NASA/LANGLEY RC-10(B)3 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILENASA/LANGLEY RC-10(B)3 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 38%c
max camber1.7% @ 32%c
LE radius1.10%c
area upper / chord0.0465
area lower / chord-0.0266
area camber / chord0.0100
TE thickness0.20%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7258-50.14353.3331.01311.671.88220ClAngle 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 0.01498% of chord; maximum error 0.06561%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
123.5
Angle at maximum lift / drag (°)
11
Minimum Cd
0.006939
Maximum Cl
1.665
Angle at maximum Cl (°)
16
Cd at zero lift
0.006959
Cm at zero angle
0.0005223
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…