Airfoils.Pro
database / Drela AG / AG45c -03f
CAMBEREDDRELA AGSELIG-DATABASETHIN

AG45c -03f

Cambered · 7% thick · low-to-mid Re
Compare↓ Download
PROFILEAG45c -03f
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.9% @ 23%c
max camber2.6% @ 38%c
LE radius0.53%c
area upper / chord0.0413
area lower / chord-0.0005
area camber / chord0.0204
TE thickness0.09%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7314-50.23.3331.13111.672.06320ClAngle 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.

Geometry fit: RMS error 0.01429% of chord; maximum error 0.06484%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
133.5
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006205
Maximum Cl
1.83
Angle at maximum Cl (°)
17
Cd at zero lift
0.006223
Cm at zero angle
-0.02882
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…