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Eiffel 10 (Wright)

Cambered · 3% thick · low-to-mid Re
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PROFILEEiffel 10 (Wright)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness2.7% @ 0%c
max camber6.2% @ 40%c
LE radius0.08%c
area upper / chord0.0509
area lower / chord0.0336
area camber / chord0.0423
TE thickness0.64%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1352-50.27553.3330.686311.671.09720ClAngle 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 0.1649% of chord; maximum error 0.7372%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
44.78
Angle at maximum lift / drag (°)
0
Minimum Cd
0.01432
Maximum Cl
0.9944
Angle at maximum Cl (°)
16
Cd at zero lift
0.07264
Cm at zero angle
-0.1014
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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