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ARA-D 10% AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEARA-D 10% AIRFOIL
surfacecamber line
BEST-FIT POLARRe 102k · M 0.09 · final
15 solved pointsM 0.09
(L/D)max19.0
α @ (L/D)max2.0°
Cd,min0.0211
Cl @ Cd,min0.37
Cd₀ (Cl=0)0.0439
Cl,max0.75
α @ Cl,max15.0°
Cm,0-0.04
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
max thickness10.0% @ 25%c
max camber4.0% @ 35%c
LE radius1.10%c
area upper / chord0.0637
area lower / chord-0.0100
area camber / chord0.0268
TE thickness1.50%c
DOWNLOAD COORDINATES
15 solved pointsM 0.09
0.00.20.40.60.8-5051015angle of attack α [deg]
Cl
POLARSbest-fitpost-stall → URANS
SOLVER WORK0 conditions · 0 engine jobs
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