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DSMA-523A AIRFOIL

Cambered · 11% thick · low-to-mid Re
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PROFILEDSMA-523A AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 35%c
max camber2.3% @ 82%c
LE radius1.33%c
area upper / chord0.0440
area lower / chord-0.0301
area camber / chord0.0070
TE thickness-0.02%c
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Polars

Preliminary
NeuralFoil
-0.4334-50.48183.3331.39711.672.31220ClAngle 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 0.03861% of chord; maximum error 0.1839%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
151.3
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007024
Maximum Cl
2.083
Angle at maximum Cl (°)
16
Cd at zero lift
0.007138
Cm at zero angle
-0.1231
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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