Airfoils.Pro
database / SD series / SD8000-089-88
CAMBEREDSD SERIESSELIG-DATABASE

SD8000-089-88

Cambered · 9% thick · low-to-mid Re
Compare↓ Download
PROFILESD8000-089-88
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.9% @ 29%c
max camber1.7% @ 49%c
LE radius0.86%c
area upper / chord0.0413
area lower / chord-0.0171
area camber / chord0.0121
TE thickness-0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5326-50.04333.3330.619211.671.19520ClAngle 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 0.01524% of chord; maximum error 0.08584%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
127.9
Angle at maximum lift / drag (°)
5
Minimum Cd
0.005993
Maximum Cl
1.051
Angle at maximum Cl (°)
7
Cd at zero lift
0.005995
Cm at zero angle
-0.05583
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…