Airfoil Tools
Search 1638 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

Airfoil Comparison

Select airfoils from the airfoil database or add your own airfoils and compare the airfoil shape and lift/drag polars.


Airfoil comparison (ah94w301-il,goe507-il,sg6043-il,goe758-il,fx73cl1152-il,sg6051-il,mh61-il,fx66h60-il,s4062-il,goe442-il,goe286-il)
Open full size plan in new window Open paginated plan in new window  
Download PDF file SVG image as text file  
 Clear all

    (ah94w301-il) AH 94-W-301

Althaus AH 94-W-301 airfoil for use on wind turbines (W)
Max thickness 30.1% at 30.9% chord
Max camber 1.3% at 80.4% chord
Remove
Airfoil details
Airfoil plotter

    (goe507-il) GOE 507 AIRFOIL

Gottingen 507 airfoil
Max thickness 8.7% at 30% chord
Max camber 2.9% at 40% chord
Remove
Airfoil details
Airfoil plotter

    (sg6043-il) SG6043

Selig / Giguere SG6043 wind turbine airfoil (high L/D)
Max thickness 10% at 32.1% chord
Max camber 5.1% at 53.3% chord
Remove
Airfoil details
Airfoil plotter

    (goe758-il) GOE 758 AIRFOIL

Gottingen 758 airfoil
Max thickness 13.9% at 30% chord
Max camber 4.7% at 40% chord
Remove
Airfoil details
Airfoil plotter

    (fx73cl1152-il) FX 73-CL1-152

Wortmann FX 73-CL1-152 airfoil
Max thickness 15.2% at 22.2% chord
Max camber 6.1% at 33.9% chord
Remove
Airfoil details
Airfoil plotter

    (sg6051-il) SG6051

Selig / Giguere SG6051 wind turbine airfoil
Max thickness 12% at 35.7% chord
Max camber 3.1% at 49.9% chord
Remove
Airfoil details
Airfoil plotter

    (mh61-il) MH 61 10.26%

Martin Hepperle MH 61 for flying wings
Max thickness 10.2% at 27.6% chord
Max camber 1.4% at 37.3% chord
Remove
Airfoil details
Airfoil plotter

    (fx66h60-il) FX 66-H-60

Wortmann FX 66-H-60 airfoil
Max thickness 6% at 22.2% chord
Max camber 1.7% at 17% chord
Remove
Airfoil details
Airfoil plotter

    (s4062-il) S4062-095-87

Selig S4062 low Reynolds number airfoil
Max thickness 9.5% at 31.7% chord
Max camber 4% at 50.4% chord
Remove
Airfoil details
Airfoil plotter

    (goe442-il) GOE 442 AIRFOIL

Gottingen 442 airfoil
Max thickness 7.7% at 19.9% chord
Max camber 4.3% at 39.9% chord
Remove
Airfoil details
Airfoil plotter

    (goe286-il) GOE 286 AIRFOIL

Gottingen 286 airfoil
Max thickness 9.4% at 29.9% chord
Max camber 4.1% at 29.9% chord
Remove
Airfoil details
Airfoil plotter

Drawing Options

Chord width in millimetres
Draw the camber line
X grid size in millimetres
Y grid size in millimetres
Used for printing plan. A4 landscape approx 280mm
Used for printing plan. A4 landscape approx 180mm

Polars for (ah94w301-il,goe507-il,sg6043-il,goe758-il,fx73cl1152-il,sg6051-il,mh61-il,fx66h60-il,s4062-il,goe442-il,goe286-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah94w301-il50,00093.3 at α=-3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il50,00054.2 at α=13.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah94w301-il100,00096.6 at α=0°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il100,000523.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah94w301-il200,000941.7 at α=12.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il200,000549.2 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   ah94w301-il500,000977.5 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il500,000576.9 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah94w301-il1,000,0009103 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah94w301-il1,000,000599 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe507-il50,000937.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il50,000538 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe507-il100,000955.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il100,000553.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe507-il200,000973.8 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il200,000567.4 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe507-il500,000995.1 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il500,000582 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe507-il1,000,0009106.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il1,000,000589.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6043-il50,000939.7 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6043-il50,000537.9 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6043-il100,000966.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6043-il100,000565.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6043-il200,000998 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6043-il200,000594.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6043-il500,0009143 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6043-il500,0005129.8 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6043-il1,000,0009175.2 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6043-il1,000,0005145.2 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe758-il50,00097.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il50,000525.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe758-il100,000945.4 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il100,000552.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe758-il200,000973.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il200,000575.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe758-il500,0009108.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il500,0005102.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe758-il1,000,0009133.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe758-il1,000,0005123.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73cl1152-il50,00094.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73cl1152-il50,000520.7 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73cl1152-il100,000924.5 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73cl1152-il100,000542.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73cl1152-il200,000953.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73cl1152-il200,000568.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73cl1152-il500,0009100.8 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73cl1152-il500,0005106.5 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73cl1152-il1,000,0009137.4 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73cl1152-il1,000,0005136.8 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6051-il50,000935.8 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il50,000534.3 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6051-il100,000958.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il100,000557.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6051-il200,000982.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il200,000578.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6051-il500,0009113 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il500,0005102.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6051-il1,000,0009133.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6051-il1,000,0005115.8 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh61-il50,000931.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il50,000533 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   mh61-il100,000947.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il100,000547.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh61-il200,000963.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il200,000560.4 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   mh61-il500,000984.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il500,000576.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh61-il1,000,000998 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh61-il1,000,000586.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66h60-il50,000928.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il50,000529.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66h60-il100,000937.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il100,000540.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66h60-il200,000951.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il200,000551.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66h60-il500,000969.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il500,000567.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx66h60-il1,000,000984.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx66h60-il1,000,000576.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s4062-il50,000938.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il50,000538.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s4062-il100,000962.7 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il100,000561.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s4062-il200,000990.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il200,000586.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s4062-il500,0009128.5 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il500,0005114.5 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s4062-il1,000,0009155 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4062-il1,000,0005131 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe442-il50,000935.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il50,000540.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe442-il100,000954.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il100,000557.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe442-il200,000973.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il200,000573 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe442-il500,000997.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il500,000593 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe442-il1,000,0009115 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe442-il1,000,0005106.2 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe286-il50,000927.9 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il50,000537.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe286-il100,000952.2 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il100,000554.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe286-il200,000972.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il200,000565.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe286-il500,000983.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il500,000578.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe286-il1,000,000995.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe286-il1,000,000589.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit