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AS5045 (15%)

Cambered · 15% thick · low-to-mid Re
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PROFILEAS5045 (15%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.0% @ 37%c
max camber1.0% @ 27%c
LE radius2.48%c
area upper / chord0.0561
area lower / chord-0.0384
area camber / chord0.0088
TE thickness0.25%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5553-50.077113.3330.709511.671.34220ClAngle 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.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.01989% of chord; maximum error 0.05746%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
132.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006765
Maximum Cl
1.184
Angle at maximum Cl (°)
7
Cd at zero lift
0.006776
Cm at zero angle
-0.06046
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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