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AH-6-40-7 AIRFOIL

Cambered · 7% thick · low-to-mid Re
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PROFILEAH-6-40-7 AIRFOIL
surfacecamber line
BEST-FIT POLARRe 102k · M 0.09 · final
12 solved pointsM 0.09
(L/D)max52.4
α @ (L/D)max8.0°
Cd,min0.0186
Cl @ Cd,min0.74
Cd₀ (Cl=0)0.0509
Cl,max1.31
α @ Cl,max12.0°
Cm,0-0.05
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
max thickness6.9% @ 20%c
max camber5.5% @ 40%c
LE radius0.52%c
area upper / chord0.0607
area lower / chord0.0155
area camber / chord0.0381
TE thickness0.70%c
DOWNLOAD COORDINATES
12 solved pointsM 0.09
-0.20.00.20.40.60.81.01.21.4-5051015angle of attack α [deg]
Cl
POLARSbest-fitpost-stall → URANS
SOLVER WORK0 conditions · 0 engine jobs
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