database / Aircraft and classic / B737C

AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASE

B737C

Cambered · 10% thick · low-to-mid Re

PROFILEB737C

surfacecamber line

BEST-FIT POLARRe 102k · M 0.09 · final

6 solved pointsM 0.09

(L/D)max14.5

α @ (L/D)max3.0°

Cd,min0.0188

Cl @ Cd,min0.10

Cd₀ (Cl=0)0.0196

Cl,max0.36

α @ Cl,max3.0°

Cm,0-0.02

fit is derived from stored OpenFOAM evidence only

GEOMETRY · AREA METRICS▾

max thickness10.0% @ 39%c

max camber1.4% @ 21%c

LE radius1.10%c

area upper / chord0.0421

area lower / chord-0.0240

area camber / chord0.0090

TE thickness0.10%c

DOWNLOAD COORDINATES

6 solved pointsM 0.09

Cl

POLARSbest-fit

SOLVER WORK0 conditions · 0 engine jobs

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