database / Aircraft and classic / B737A

AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASETHICK

B737A

Cambered · 15% thick · low-to-mid Re

PROFILEB737A

surfacecamber line

BEST-FIT POLARRe 102k · M 0.09 · final

8 solved pointsM 0.09

(L/D)max2.6

α @ (L/D)max2.0°

Cd,min0.0316

Cl @ Cd,min0.03

Cd₀ (Cl=0)0.0333

Cl,max0.34

α @ Cl,max11.0°

Cm,00.01

fit is derived from stored OpenFOAM evidence only

GEOMETRY · AREA METRICS▾

max thickness15.4% @ 20%c

max camber1.9% @ 5%c

LE radius2.60%c

area upper / chord0.0581

area lower / chord-0.0400

area camber / chord0.0090

TE thickness0.06%c

DOWNLOAD COORDINATES

8 solved pointsM 0.09

Cl

POLARSbest-fitpost-stall → URANS

SOLVER WORK0 conditions · 0 engine jobs

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