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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG10

Cambered · 5% thick · low-to-mid Re
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PROFILEAG10
surfacecamber line
GEOMETRY · AREA METRICS
max thickness4.7% @ 16%c
max camber1.7% @ 33%c
LE radius0.25%c
area upper / chord0.0262
area lower / chord-0.0039
area camber / chord0.0111
TE thickness0.36%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6432-50.24263.3331.12811.672.01420ClAngle 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 0.008982% of chord; maximum error 0.04287%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
128.5
Angle at maximum lift / drag (°)
9
Minimum Cd
0.00626
Maximum Cl
1.793
Angle at maximum Cl (°)
16
Cd at zero lift
0.00628
Cm at zero angle
-0.02951
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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