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AH 88-K-136/16

Cambered · 14% thick · low-to-mid Re
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PROFILEAH 88-K-136/16
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.5% @ 44%c
max camber3.1% @ 37%c
LE radius2.02%c
area upper / chord0.0645
area lower / chord-0.0289
area camber / chord0.0178
TE thickness0.03%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5064-50.11433.3330.734911.671.35620ClAngle 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 0.04508% of chord; maximum error 0.2769%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
116.1
Angle at maximum lift / drag (°)
8
Minimum Cd
0.006682
Maximum Cl
1.2
Angle at maximum Cl (°)
10
Cd at zero lift
0.006698
Cm at zero angle
-0.02769
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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