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Airfoil database search

Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.

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(mh43-il) MH 43 8.5%

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MH 43  8.5%Martin Hepperle MH 43 for F3B and F3E
Max thickness 8.5% at 31.4% chord
Max camber 1.7% at 36.4% chord
Max Cl/Cd 86.9 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(usa27m2-il) USA 27 mod. AIRFOIL

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USA 27 mod. AIRFOILUSA-27MOD airfoil
Max thickness 13.3% at 30% chord
Max camber 5% at 40% chord
Max Cl/Cd 86.8 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(goe210-il) GOE 210 (DAIMLER) AIRFOIL

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GOE 210 (DAIMLER) AIRFOILGottingen 210 (DAIMLER) airfoil
Max thickness 6.6% at 30% chord
Max camber 4.3% at 40% chord
Max Cl/Cd 86.8 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(goe595-il) GOE 595 AIRFOIL

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GOE 595 AIRFOILGottingen 595 airfoil
Max thickness 9.6% at 30% chord
Max camber 3% at 40% chord
Max Cl/Cd 86.8 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(goe143-il) GOE 143 (MVA H.20) AIRFOIL

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GOE 143 (MVA H.20) AIRFOILGottingen 143 (MVA H.20) airfoil
Max thickness 7.4% at 19.9% chord
Max camber 3.8% at 29.9% chord
Max Cl/Cd 86.8 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(hq3013-il) HQ 3.0/13 AIRFOIL

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HQ 3.0/13 AIRFOILQuabeck HQ 3.0/13 R/C sailplane airfoil
Max thickness 13% at 35% chord
Max camber 3% at 50% chord
Max Cl/Cd 86.8 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(goe147-il) GOE 147 (MVA H.6) AIRFOIL

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GOE 147 (MVA H.6) AIRFOILGottingen 147 (MVA H.6) airfoil
Max thickness 7.5% at 14.9% chord
Max camber 3.8% at 29.9% chord
Max Cl/Cd 86.8 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(goe113-il) GOE 113 AIRFOIL

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GOE 113 AIRFOILGottingen 113 airfoil
Max thickness 6.7% at 30% chord
Max camber 3% at 40% chord
Max Cl/Cd 86.8 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(hq158-il) HQ 1.5/8 AIRFOIL

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HQ 1.5/8 AIRFOILQuabeck HQ 1.5/8 R/C sailplane airfoil
Max thickness 8% at 32.5% chord
Max camber 1.5% at 50% chord
Max Cl/Cd 86.8 at Re# 500,000
Source UIUC Airfoil Coordinates Database

(m12-il) NACA M12 AIRFOIL

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NACA M12 AIRFOILNACA/Munk M-12 airfoil
Max thickness 11.9% at 30% chord
Max camber 2% at 30% chord
Max Cl/Cd 86.7 at Re# 500,000
Source UIUC Airfoil Coordinates Database
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