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AH 79-100 C

Cambered · 10% thick · low-to-mid Re
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PROFILEAH 79-100 C
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.9% @ 31%c
max camber6.7% @ 50%c
LE radius1.09%c
area upper / chord0.0813
area lower / chord0.0122
area camber / chord0.0467
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.2521-50.82763.3331.40311.671.97920ClAngle 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 0.01418% of chord; maximum error 0.05893%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
168.9
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006703
Maximum Cl
1.835
Angle at maximum Cl (°)
8
Cd at zero lift
—
Cm at zero angle
-0.2404
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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