Airfoils.Pro
database / Drela AG / AG52
CAMBEREDDRELA AGSELIG-DATABASE

AG52

Cambered · 8% thick · low-to-mid Re
↓ Download
PROFILEAG52
surfacecamber line
BEST-FIT POLARRe 102k · M 0.09 · final
12 solved pointsM 0.09
(L/D)max19.3
α @ (L/D)max2.5°
Cd,min0.0166
Cl @ Cd,min0.21
Cd₀ (Cl=0)0.0205
Cl,max0.60
α @ Cl,max6.5°
Cm,0-0.04
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
max thickness8.4% @ 28%c
max camber1.8% @ 41%c
LE radius0.77%c
area upper / chord0.0400
area lower / chord-0.0155
area camber / chord0.0122
TE thickness0.04%c
DOWNLOAD COORDINATES
12 solved pointsM 0.09
-0.20.00.20.40.6-4-202468angle of attack α [deg]
Cl
POLARSbest-fit
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…