Airfoils.Pro
database / Other families / Apex 16 (normalized
CAMBEREDOTHER FAMILIESSELIG-DATABASE

Apex 16 (normalized

Cambered · 13% thick · low-to-mid Re
↓ Download
PROFILEApex 16 (normalized
surfacecamber line
BEST-FIT POLARRe 102k · M 0.09 · final
15 solved pointsM 0.09
(L/D)max17.4
α @ (L/D)max2.5°
Cd,min0.0197
Cl @ Cd,min0.24
Cd₀ (Cl=0)0.0256
Cl,max0.84
α @ Cl,max14.0°
Cm,0-0.06
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
max thickness12.9% @ 37%c
max camber2.7% @ 58%c
LE radius1.84%c
area upper / chord0.0619
area lower / chord-0.0227
area camber / chord0.0196
TE thickness0.00%c
DOWNLOAD COORDINATES
15 solved pointsM 0.09
-0.20.00.20.40.60.8-4-202468101214angle of attack α [deg]
Cl
POLARSbest-fitpost-stall → URANS
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…