Airfoils.Pro
database / Aircraft and classic / B737D
AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASE

B737D

Cambered · 11% thick · low-to-mid Re
↓ Download
PROFILEB737D
surfacecamber line
BEST-FIT POLARRe 102k · M 0.09 · final
7 solved pointsM 0.09
(L/D)max14.0
α @ (L/D)max4.0°
Cd,min0.0201
Cl @ Cd,min0.07
Cd₀ (Cl=0)0.0209
Cl,max0.43
α @ Cl,max4.0°
Cm,0-0.02
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
max thickness10.8% @ 40%c
max camber1.6% @ 21%c
LE radius1.28%c
area upper / chord0.0460
area lower / chord-0.0256
area camber / chord0.0102
TE thickness0.16%c
DOWNLOAD COORDINATES
7 solved pointsM 0.09
-0.3-0.2-0.10.00.10.20.30.4-5-4-3-2-101234angle of attack α [deg]
Cl
POLARSbest-fit
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…