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US1000ROOT

Symmetric · 19% thick · low-to-mid Re
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PROFILEUS1000ROOT
surfacecamber line
GEOMETRY · AREA METRICS
max thickness18.6% @ 27%c
max camber0.1% @ 0%c
LE radius3.80%c
area upper / chord0.0593
area lower / chord-0.0593
area camber / chord0.0000
TE thickness0.01%c
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Polars

Preliminary
NeuralFoil
-0.8077-5-0.047913.3330.711911.671.47220ClAngle 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 0.02571% of chord; maximum error 0.08965%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
112.3
Angle at maximum lift / drag (°)
9
Minimum Cd
0.007271
Maximum Cl
1.282
Angle at maximum Cl (°)
11
Cd at zero lift
0.007271
Cm at zero angle
0.0002265
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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