Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

FX 71-L-150/30 AIRFOIL (fx71l150-il)

FX 71-L-150/30 AIRFOIL - Wortmann FX 71-L-150/30 airfoil


Airfoil fx71l150-il
Details Dat file Parser  
(fx71l150-il) FX 71-L-150/30 AIRFOIL
Wortmann FX 71-L-150/30 airfoil
Max thickness 15% at 33.9% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FX 71-L-150/30 AIRFOIL
       44.       44.

0	0
.00107	.00813
.00428	.01437
.00961	.01896
.01704	.02442
.02653	.02945
.03806	.03465
.05156	.03958
.06699	.0445
.08427	.04902
.10332	.05354
.12408	.05753
.14645	.06136
.17033	.06467
.19562	.06774
.22221	.07014
.25	.07229
.27886	.07369
.30866	.07477
.33928	.075
.37059	.07486
.40245	.07372
.43474	.07219
.4673	.06969
.5	.06667
.5327	.06271
.56526	.05845
.59755	.05363
.62941	.0485
.66072	.04264
.69134	.03729
.72114	.0314
.75	.02742
.77779	.02347
.80438	.0204
.82967	.01709
.85355	.01448
.87592	.01177
.91573	.00756
.94844	.00435
.97347	.00227
.99039	.00089
.99893	.0001
1	0

0	0
.00107	-.00813
.00428	-.01437
.00961	-.01896
.01704	-.02442
.02653	-.02945
.03806	-.03465
.05156	-.03958
.06699	-.0445
.08427	-.04902
.10332	-.05354
.12408	-.05753
.14645	-.06136
.17033	-.06467
.19562	-.06774
.22221	-.07014
.25	-.07229
.27886	-.07369
.30866	-.07477
.33928	-.075
.37059	-.07486
.40245	-.07372
.43474	-.07219
.4673	-.06969
.5	-.06667
.5327	-.06271
.56526	-.05845
.59755	-.05363
.62941	-.0485
.66072	-.04264
.69134	-.03729
.72114	-.0314
.75	-.02742
.77779	-.02347
.80438	-.0204
.82967	-.01709
.85355	-.01448
.87592	-.01177
.91573	-.00756
.94844	-.00435
.97347	-.00227
.99039	-.00089
.99893	-.0001
1	0
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

FX 71-L-150/20 AIRFOILPreviewDetails
FX 71-L-150/25 AIRFOILPreviewDetails
FX 71-L-150/30 AIRFOILPreviewDetails
NACA 63-015A AIRFOILPreviewDetails
NACA 642-015 AIRFOILPreviewDetails
WORTMANN FX L V-152 AIRFOILPreviewDetails
EPPLER 520 AIRFOILPreviewDetails
NACA 0015PreviewDetails
NACA 642-015A AIRFOILPreviewDetails
LWK 80-150/K25PreviewDetails

Polars for FX 71-L-150/30 AIRFOIL (fx71l150-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx71l150-il50,000927.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   fx71l150-il50,000526.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx71l150-il100,000939.5 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx71l150-il100,000535.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx71l150-il200,000947.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   fx71l150-il200,000540.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx71l150-il500,000951.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx71l150-il500,000549.1 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   fx71l150-il1,000,000959.2 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   fx71l150-il1,000,000558.3 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit