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ARA-D 6% AIRFOIL

Cambered · 6% thick · low-to-mid Re
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PROFILEARA-D 6% AIRFOIL
surfacecamber line
BEST-FIT POLARRe 102k · M 0.09 · final
10 solved pointsM 0.09
(L/D)max41.2
α @ (L/D)max5.0°
Cd,min0.0201
Cl @ Cd,min0.69
Cd₀ (Cl=0)0.0443
Cl,max0.92
α @ Cl,max5.0°
Cm,0-0.06
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
max thickness6.0% @ 20%c
max camber5.0% @ 45%c
LE radius0.40%c
area upper / chord0.0575
area lower / chord0.0106
area camber / chord0.0341
TE thickness1.10%c
DOWNLOAD COORDINATES
10 solved pointsM 0.09
0.00.20.40.60.8-4-2024angle of attack α [deg]
Cl
POLARSbest-fit
SOLVER WORK0 conditions · 0 engine jobs
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