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AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASE

P-51D TIP (BL215)

Cambered · 11% thick · low-to-mid Re
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PROFILEP-51D TIP (BL215)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.4% @ 46%c
max camber1.3% @ 46%c
LE radius1.43%c
area upper / chord0.0448
area lower / chord-0.0282
area camber / chord0.0083
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.6283-5-0.027563.3330.573211.671.17420ClAngle 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 0.03209% of chord; maximum error 0.1317%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
120.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006073
Maximum Cl
1.024
Angle at maximum Cl (°)
7
Cd at zero lift
0.006076
Cm at zero angle
-0.03565
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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