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cr001sm

Cambered · 7% thick · low-to-mid Re
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PROFILEcr001sm
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.3% @ 27%c
max camber4.1% @ 46%c
LE radius0.59%c
area upper / chord0.0525
area lower / chord0.0041
area camber / chord0.0283
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1882-50.38753.3330.963211.671.53920ClAngle 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.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.008288% of chord; maximum error 0.03041%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
145.1
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006542
Maximum Cl
1.395
Angle at maximum Cl (°)
7
Cd at zero lift
0.007105
Cm at zero angle
-0.131
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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