(goe421-il) GOE 421 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| Gottingen 421 airfoil Max thickness 19% at 29.3% chord Max camber 8.1% at 49.3% chord Max Cl/Cd 76.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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(usa31-il) USA 31 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| USA-31 airfoil Max thickness 14.8% at 19.7% chord Max camber 9.3% at 39.7% chord Max Cl/Cd 69.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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(usa32-il) USA 32 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| USA-32 airfoil Max thickness 14.7% at 19.8% chord Max camber 9.3% at 39.8% chord Max Cl/Cd 68.9 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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(goe531-il) GOE 531 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| Gottingen 531 airfoil Max thickness 13.8% at 19.5% chord Max camber 14.7% at 49.3% chord Max Cl/Cd 67.5 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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(goe531-il) GOE 531 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| Gottingen 531 airfoil Max thickness 13.8% at 19.5% chord Max camber 14.7% at 49.3% chord Max Cl/Cd 66.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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(goe481-il) GOE 481 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| Gottingen 481 airfoil Max thickness 13.4% at 9.6% chord Max camber 8.8% at 39.4% chord Max Cl/Cd 63.4 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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(usa32-il) USA 32 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| USA-32 airfoil Max thickness 14.7% at 19.8% chord Max camber 9.3% at 39.8% chord Max Cl/Cd 59.6 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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(goe481-il) GOE 481 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| Gottingen 481 airfoil Max thickness 13.4% at 9.6% chord Max camber 8.8% at 39.4% chord Max Cl/Cd 58.3 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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(goe571-il) GOE 571 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| Gottingen 571 airfoil Max thickness 24.9% at 29.4% chord Max camber 9.8% at 29.4% chord Max Cl/Cd 56.1 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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(goe561-il) GOE 561 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
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| Gottingen 561 airfoil Max thickness 25% at 29.8% chord Max camber 10.2% at 29.8% chord Max Cl/Cd 43.2 at Re# 500,000 Source UIUC Airfoil Coordinates Database
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