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AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASETHICK

P-51D ROOT (BL17.5)

Cambered · 17% thick · low-to-mid Re
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PROFILEP-51D ROOT (BL17.5)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.5% @ 38%c
max camber1.3% @ 68%c
LE radius3.00%c
area upper / chord0.0617
area lower / chord-0.0436
area camber / chord0.0091
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6432-50.2253.3331.09311.671.96120ClAngle 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 0.03994% of chord; maximum error 0.1315%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
123.7
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007685
Maximum Cl
1.744
Angle at maximum Cl (°)
16
Cd at zero lift
0.007699
Cm at zero angle
-0.04185
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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