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AMES01

Cambered · 10% thick · low-to-mid Re
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PROFILEAMES01
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.3% @ 35%c
max camber1.4% @ 15%c
LE radius1.16%c
area upper / chord0.0453
area lower / chord-0.0285
area camber / chord0.0084
TE thickness0.60%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7872-50.14683.3331.08111.672.01520ClAngle 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 0.01145% of chord; maximum error 0.03314%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
124.9
Angle at maximum lift / drag (°)
11
Minimum Cd
0.007064
Maximum Cl
1.781
Angle at maximum Cl (°)
17
Cd at zero lift
0.007098
Cm at zero angle
0.004552
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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