Airfoils.Pro
database / Research / NLR-1T AIRFOIL
CAMBEREDRESEARCHSELIG-DATABASE

NLR-1T AIRFOIL

Cambered · 9% thick · low-to-mid Re
Compare↓ Download
PROFILENLR-1T AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.7% @ 38%c
max camber1.3% @ 22%c
LE radius0.83%c
area upper / chord0.0414
area lower / chord-0.0236
area camber / chord0.0089
TE thickness0.21%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6967-50.17373.3331.04411.671.91520ClAngle 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 0.01708% of chord; maximum error 0.06323%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
122.4
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006688
Maximum Cl
1.697
Angle at maximum Cl (°)
16
Cd at zero lift
0.006744
Cm at zero angle
-0.007908
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…