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DF 101 AIRFOIL

Cambered · 11% thick · low-to-mid Re
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PROFILEDF 101 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 29%c
max camber2.3% @ 43%c
LE radius1.33%c
area upper / chord0.0522
area lower / chord-0.0215
area camber / chord0.0153
TE thickness0.01%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5285-50.30473.3331.13811.671.97120ClAngle of attack (°)
Why this curve

This is a NeuralFoil prediction from the stored profile coordinates and the selected flow condition, with AeroSandbox compressibility corrections. It is not a completed OpenFOAM calculation.

Prediction error has not been calibrated for this condition. No accuracy interval is claimed.

Geometry fit: RMS error 0.01519% of chord; maximum error 0.09255%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
129.4
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006944
Maximum Cl
1.763
Angle at maximum Cl (°)
16
Cd at zero lift
0.006946
Cm at zero angle
-0.05082
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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