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Airfoil database list (O).

ONERA OA206 AIRFOIL to OAF139 AIRFOIL

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(oa206-il) ONERA OA206 AIRFOIL

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ONERA OA206 AIRFOILONERA/Aerospatiale OA206 rotorcraft airfoil (Constructed from patent and smoothed)
Max thickness 6% at 31.8% chord
Max camber 0.8% at 19.6% chord
Source UIUC Airfoil Coordinates Database

(oa209-il) ONERA OA209 AIRFOIL

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ONERA OA209 AIRFOILONERA/Aerospatiale OA209 rotorcraft airfoil (Constructed from patent and smoothed)
Max thickness 9% at 29.3% chord
Max camber 1.6% at 17.1% chord
Source UIUC Airfoil Coordinates Database

(oa212-il) ONERA OA212 AIRFOIL

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ONERA OA212 AIRFOILONERA/Aerospatiale OA212 rotorcraft airfoil (Constructed from patent and smoothed)
Max thickness 12% at 31.8% chord
Max camber 2.3% at 31.8% chord
Source UIUC Airfoil Coordinates Database

(oa213-il) ONERA OA213 AIRFOIL

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ONERA OA213 AIRFOILONERA/Aerospatiale OA213 rotorcraft airfoil (Constructed from patent and smoothed)
Max thickness 12.6% at 32.5% chord
Max camber 3.3% at 25% chord
Source UIUC Airfoil Coordinates Database

(oaf095-il) OAF095 AIRFOIL

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OAF095 AIRFOILONERA/Aerospatiale OAF095 Fenestron airfoil
Max thickness 9.5% at 23.2% chord
Max camber 3.9% at 53.1% chord
Source UIUC Airfoil Coordinates Database

(oaf102-il) OAF102 AIRFOIL

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OAF102 AIRFOILONERA/Aerospatiale OAF102 Fenestron airfoil
Max thickness 10.2% at 28.7% chord
Max camber 3.6% at 53.1% chord
Source UIUC Airfoil Coordinates Database

(oaf117-il) OAF117 AIRFOIL

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OAF117 AIRFOILONERA/Aerospatiale OAF117 Fenestron airfoil
Max thickness 11.5% at 23.2% chord
Max camber 2% at 46.9% chord
Source UIUC Airfoil Coordinates Database

(oaf128-il) OAF128 AIRFOIL

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OAF128 AIRFOILONERA/Aerospatiale OAF128 Fenestron airfoil
Max thickness 12.8% at 23.2% chord
Max camber 1% at 43.7% chord
Source UIUC Airfoil Coordinates Database

(oaf139-il) OAF139 AIRFOIL

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OAF139 AIRFOILONERA/Aerospatiale OAF139 Fenestron airfoil
Max thickness 13.7% at 23.2% chord
Max camber 0% at 0.1% chord
Source UIUC Airfoil Coordinates Database
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