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AH 95-160

Cambered · 16% thick · low-to-mid Re
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PROFILEAH 95-160
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.0% @ 38%c
max camber5.5% @ 44%c
LE radius2.82%c
area upper / chord0.0874
area lower / chord-0.0176
area camber / chord0.0349
TE thickness0.22%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1029-50.57553.3331.25411.671.93220ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 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 0.007273% of chord; maximum error 0.02068%.

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

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
148
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006932
Maximum Cl
1.763
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.148
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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