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AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASETHICK

P51HROOT

Cambered · 15% thick · low-to-mid Re
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PROFILEP51HROOT
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.5% @ 45%c
max camber1.3% @ 47%c
LE radius2.65%c
area upper / chord0.0613
area lower / chord-0.0435
area camber / chord0.0089
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.6236-5-0.019763.3330.584111.671.18820ClAngle 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 0.02458% of chord; maximum error 0.08635%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
111.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006985
Maximum Cl
1.037
Angle at maximum Cl (°)
8
Cd at zero lift
0.006998
Cm at zero angle
-0.03329
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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