Airfoils.Pro
database / Other families / MARSKE4
CAMBEREDOTHER FAMILIESSELIG-DATABASE

MARSKE4

Cambered · 10% thick · low-to-mid Re
Compare↓ Download
PROFILEMARSKE4
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.2% @ 21%c
max camber2.8% @ 15%c
LE radius1.14%c
area upper / chord0.0463
area lower / chord-0.0239
area camber / chord0.0112
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6809-5-0.04783.3330.585311.671.21820ClAngle 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 0.05104% of chord; maximum error 0.3052%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
113.5
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006353
Maximum Cl
1.06
Angle at maximum Cl (°)
20
Cd at zero lift
0.006437
Cm at zero angle
0.02797
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…