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NASA/LANGLEY RC08-64C AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILENASA/LANGLEY RC08-64C AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.0% @ 40%c
max camber1.0% @ 35%c
LE radius0.70%c
area upper / chord0.0352
area lower / chord-0.0227
area camber / chord0.0063
TE thickness0.16%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7033-50.1783.3331.05911.671.94120ClAngle 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 0.02645% of chord; maximum error 0.22%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
126.4
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006518
Maximum Cl
1.72
Angle at maximum Cl (°)
16
Cd at zero lift
0.006524
Cm at zero angle
-0.01637
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…