Airfoils.Pro
database / Other families / GRIFFITH30SYMSUCTION
OTHER FAMILIESSELIG-DATABASESYMMETRICTHICK

GRIFFITH30SYMSUCTION

Symmetric · 31% thick · low-to-mid Re
Compare↓ Download
PROFILEGRIFFITH30SYMSUCTION
surfacecamber line
GEOMETRY · AREA METRICS
max thickness30.6% @ 49%c
max camber0.0% @ 0%c
LE radius10.29%c
area upper / chord0.1026
area lower / chord-0.1026
area camber / chord0.0000
TE thickness0.20%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.3017-50.21343.3330.728511.671.24420ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.1701% of chord; maximum error 0.4615%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
26.88
Angle at maximum lift / drag (°)
13
Minimum Cd
0.03126
Maximum Cl
1.115
Angle at maximum Cl (°)
20
Cd at zero lift
0.03646
Cm at zero angle
-1.004e-16
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…