Airfoil Tools
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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 (goe795-il,goe336-il,goe289-il,goe329-il,goe450-il,sg6050-il,mh60-il,naca633418-il,goe436-il,goe188-il,goe625-il,goe199-il,goe406-il,ah93157-il)
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    (goe795-il) GOE 795 AIRFOIL

Gottingen 795 airfoil
Max thickness 8% at 30.9% chord
Max camber 2.4% at 43.5% chord
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    (goe336-il) GOE 336 (MVA H.44) AIRFOIL

Gottingen 336 (MVA H.44) airfoil
Max thickness 9% at 29.9% chord
Max camber 5.4% at 29.9% chord
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    (goe289-il) GOE 289 (MVA 289) AIRFOIL

Gottingen 289 (MVA 289) airfoil
Max thickness 16.8% at 30% chord
Max camber 6.1% at 40% chord
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    (goe329-il) GOE 329 (PFALZ 58) AIRFOIL

Gottingen 329 (Pfalz 58) airfoil
Max thickness 10.2% at 29.9% chord
Max camber 5.5% at 29.9% chord
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    (goe450-il) GOE 450 AIRFOIL

Gottingen 450 airfoil
Max thickness 8.9% at 29.9% chord
Max camber 5.2% at 39.9% chord
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    (sg6050-il) SG6050

Selig / Giguere SG6050 wind turbine airfoil
Max thickness 16% at 31.5% chord
Max camber 3.1% at 48.9% chord
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    (mh60-il) MH 60 10.08%

Martin Hepperle MH 60 for flying wings
Max thickness 10.1% at 26.9% chord
Max camber 1.7% at 36.6% chord
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    (naca633418-il) NACA 63

NACA 63
Max thickness 18% at 33.9% chord
Max camber 2.2% at 50% chord
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    (goe436-il) GOE 436 AIRFOIL

Gottingen 436 airfoil
Max thickness 11% at 30% chord
Max camber 3.8% at 30% chord
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    (goe188-il) GOE 188 (SCHTTE-LANZ 3U10) AIRFOIL

Gottingen 188 (Schatte-Lanz 3U10) airfoil
Max thickness 8.9% at 30% chord
Max camber 4.3% at 30% chord
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    (goe625-il) GOE 625 AIRFOIL

Gottingen 625 airfoil
Max thickness 20% at 30% chord
Max camber 6.1% at 40% chord
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    (goe199-il) GOE 199 (L.F.G. 5406) AIRFOIL

Gottingen 199 (L.F.G. 5406) airfoil
Max thickness 7.3% at 30% chord
Max camber 5.2% at 30% chord
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    (goe406-il) GOE 406 AIRFOIL

Gottingen 406 airfoil
Max thickness 11.7% at 29.9% chord
Max camber 5.5% at 39.9% chord
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    (ah93157-il) AH 93-157

Althaus AH 93-157 airfoil
Max thickness 15.7% at 39.6% chord
Max camber 3.5% at 41.7% chord
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Used for printing plan. A4 landscape approx 280mm
Used for printing plan. A4 landscape approx 180mm

Polars for (goe795-il,goe336-il,goe289-il,goe329-il,goe450-il,sg6050-il,mh60-il,naca633418-il,goe436-il,goe188-il,goe625-il,goe199-il,goe406-il,ah93157-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe795-il50,000938 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795-il50,000537.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe795-il100,000956.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795-il100,000553.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe795-il200,000975.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795-il200,000567.5 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe795-il500,000995.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795-il500,000580.2 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   goe795-il1,000,0009105 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795-il1,000,000584.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe336-il50,000930.6 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe336-il50,000534.2 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe336-il100,000956.7 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe336-il100,000557.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe336-il200,000979.5 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe336-il200,000577.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe336-il500,0009107.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe336-il500,000597.9 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe336-il1,000,0009125.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe336-il1,000,000594.9 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe289-il50,00094.3 at α=11.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il50,000520.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe289-il100,000938.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il100,000546.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe289-il200,000965.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il200,000564.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe289-il500,000992.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il500,000587.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe289-il1,000,0009115.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe289-il1,000,0005109.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe329-il50,000923.6 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il50,000537.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe329-il100,000953.3 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il100,000556.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe329-il200,000973.9 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il200,000575.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe329-il500,0009104.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il500,0005103.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe329-il1,000,0009129.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe329-il1,000,0005125.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe450-il50,000939.6 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il50,000540.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe450-il100,000963.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il100,000564.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe450-il200,000988.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il200,000585.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe450-il500,0009120.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il500,0005108 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe450-il1,000,0009141.4 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe450-il1,000,0005118.9 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6050-il50,00098.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il50,000525.6 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6050-il100,000950 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il100,000552.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6050-il200,000974.7 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il200,000573.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6050-il500,0009105.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il500,000597.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sg6050-il1,000,0009126.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sg6050-il1,000,0005113 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh60-il50,000927.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il50,000532.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh60-il100,000945 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il100,000546.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh60-il200,000961.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il200,000560 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   mh60-il500,000982.8 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il500,000577.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   mh60-il1,000,000998.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   mh60-il1,000,000591 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   naca633418-il50,000920.3 at α=12.75°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il50,000516.6 at α=11.75°Mach=0 Ncrit=5Xfoil predictionDetails
   naca633418-il100,000945.4 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il100,000544.7 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   naca633418-il200,000969.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il200,000567.8 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   naca633418-il500,000999.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il500,000591.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   naca633418-il1,000,0009120.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   naca633418-il1,000,0005106.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe436-il50,000923.5 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il50,000534.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe436-il100,000947.8 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il100,000551.6 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe436-il200,000968.2 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il200,000569.1 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe436-il500,000996.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il500,000592.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe436-il1,000,0009118.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe436-il1,000,0005108.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe188-il50,000931.6 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe188-il50,000539.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe188-il100,000951.4 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe188-il100,000557.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe188-il200,000971.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe188-il200,000574.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe188-il500,000998.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe188-il500,000599 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe188-il1,000,0009119.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe188-il1,000,0005116.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe625-il50,00093.8 at α=13.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il50,000518.8 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe625-il100,000933.8 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il100,000542.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe625-il200,000958.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il200,000557.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe625-il500,000980.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il500,000577.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe625-il1,000,0009101.4 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe625-il1,000,000599.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe199-il50,000936.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe199-il50,000540.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe199-il100,000955.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe199-il100,000554.9 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe199-il200,000972 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe199-il200,000567.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe199-il500,000989.8 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe199-il500,000589.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe199-il1,000,0009108.2 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe199-il1,000,0005106.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe406-il50,000917.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il50,000534.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe406-il100,000954.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il100,000553.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe406-il200,000975.6 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il200,000568.1 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe406-il500,000994.8 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il500,000589.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe406-il1,000,0009114.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe406-il1,000,0005112 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93157-il50,00094.7 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93157-il50,000514.4 at α=12.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93157-il100,000940 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93157-il100,000537.5 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93157-il200,000974.9 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93157-il200,000566.2 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93157-il500,0009100.4 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93157-il500,000592 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   ah93157-il1,000,0009120.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah93157-il1,000,0005112.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
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