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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 744 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILEGOE 744 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.5% @ 21%c
max camber7.0% @ 30%c
LE radius2.31%c
area upper / chord0.0807
area lower / chord-0.0084
area camber / chord0.0361
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.5345-50.22383.3330.982111.671.7420ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 3 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.08249% of chord; maximum error 0.3572%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

  • · Provisional history
  • · Provisional history
  • · Provisional history

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
25.42
Angle at maximum lift / drag (°)
7
Minimum Cd
0.03842
Maximum Cl
1.551
Angle at maximum Cl (°)
19
Cd at zero lift
0.04247
Cm at zero angle
0.02532
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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