Airfoils.Pro
database / Drela AG / AG12
CAMBEREDDRELA AGSELIG-DATABASETHIN

AG12

Cambered · 6% thick · low-to-mid Re
↓ Download
PROFILEAG12
surfacecamber line
BEST-FIT POLARRe 102k · M 0.09 · final
49 solved pointsM 0.09
(L/D)max24.3
α @ (L/D)max1.5°
Cd,min0.0133
Cl @ Cd,min0.26
Cd₀ (Cl=0)0.0210
Cl,max0.97
α @ Cl,max17.0°
Cm,0-0.03
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
max thickness6.2% @ 21%c
max camber1.8% @ 43%c
LE radius0.43%c
area upper / chord0.0312
area lower / chord-0.0056
area camber / chord0.0128
TE thickness0.09%c
DOWNLOAD COORDINATES
49 solved pointsM 0.09–0.49
-0.4-0.20.00.20.40.60.81.0-505101522angle of attack α [deg]
Cl
POLARSbest-fitalternate stored result · not in best-fitneeds URANS confirmationpost-stall → URANS
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…