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Falcon

Cambered · 14% thick · low-to-mid Re
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PROFILEFalcon
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.7% @ 31%c
max camber1.6% @ 21%c
LE radius2.06%c
area upper / chord0.0553
area lower / chord-0.0383
area camber / chord0.0085
TE thickness0.29%c
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Polars

Preliminary
NeuralFoil
-0.7029-5-0.0030693.3330.696711.671.39720ClAngle 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 0.03456% of chord; maximum error 0.1064%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
122.6
Angle at maximum lift / drag (°)
8
Minimum Cd
0.006815
Maximum Cl
1.222
Angle at maximum Cl (°)
9
Cd at zero lift
0.006821
Cm at zero angle
-0.009177
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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