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

AVISTAR

Cambered · 15% thick · low-to-mid Re
Compare↓ Download
PROFILEAVISTAR
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.5% @ 35%c
max camber2.2% @ 38%c
LE radius2.32%c
area upper / chord0.0629
area lower / chord-0.0358
area camber / chord0.0135
TE thickness0.32%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6096-50.042093.3330.693811.671.34520ClAngle 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 0.05484% of chord; maximum error 0.1546%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
124.5
Angle at maximum lift / drag (°)
7
Minimum Cd
0.00683
Maximum Cl
1.183
Angle at maximum Cl (°)
8
Cd at zero lift
0.006838
Cm at zero angle
-0.03605
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…