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DOA5

Cambered · 16% thick · low-to-mid Re
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PROFILEDOA5
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.2% @ 40%c
max camber2.5% @ 78%c
LE radius2.89%c
area upper / chord0.0722
area lower / chord-0.0363
area camber / chord0.0179
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.293-50.25743.3330.807711.671.35820ClAngle 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 0.05351% of chord; maximum error 0.2754%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
131.3
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007106
Maximum Cl
1.22
Angle at maximum Cl (°)
8
Cd at zero lift
0.007142
Cm at zero angle
-0.1127
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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