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AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASE

P51HTIP

Cambered · 12% thick · low-to-mid Re
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PROFILEP51HTIP
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 45%c
max camber1.3% @ 47%c
LE radius1.59%c
area upper / chord0.0497
area lower / chord-0.0320
area camber / chord0.0088
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6359-50.18463.3331.00511.671.82520ClAngle 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 0.01962% of chord; maximum error 0.07003%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
122
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007058
Maximum Cl
1.62
Angle at maximum Cl (°)
17
Cd at zero lift
0.00707
Cm at zero angle
-0.03051
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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