Airfoils.Pro
database / Other families / BOE106
CAMBEREDOTHER FAMILIESSELIG-DATABASE

BOE106

Cambered · 13% thick · low-to-mid Re
↓ Download
PROFILEBOE106
surfacecamber line
BEST-FIT POLARRe 102k · M 0.09 · final
5 solved pointsM 0.09
(L/D)max19.7
α @ (L/D)max2.0°
Cd,min0.0187
Cl @ Cd,min0.29
Cd₀ (Cl=0)0.0352
Cl,max0.43
α @ Cl,max2.0°
Cm,0-0.04
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
max thickness13.1% @ 30%c
max camber3.3% @ 40%c
LE radius1.88%c
area upper / chord0.0663
area lower / chord-0.0224
area camber / chord0.0219
TE thickness0.04%c
DOWNLOAD COORDINATES
5 solved pointsM 0.09
-0.10.00.10.20.30.4-5-4-3-2-1012angle of attack α [deg]
Cl
POLARSbest-fit
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…