Airfoils.Pro
database / Other families / AH 63-K-127/24
CAMBEREDOTHER FAMILIESSELIG-DATABASE

AH 63-K-127/24

Cambered · 13% thick · low-to-mid Re
Compare↓ Download
PROFILEAH 63-K-127/24
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.7% @ 40%c
max camber3.8% @ 44%c
LE radius1.78%c
area upper / chord0.0662
area lower / chord-0.0166
area camber / chord0.0248
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2582-50.34983.3330.957811.671.56620ClAngle 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 0.04346% of chord; maximum error 0.1862%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
150.2
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006411
Maximum Cl
1.414
Angle at maximum Cl (°)
8
Cd at zero lift
0.006425
Cm at zero angle
-0.1111
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…