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(oa206il) ONERA OA206 AIRFOIL Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file ONERA/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 (oa209il) ONERA OA209 AIRFOIL Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file ONERA/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 (oa212il) ONERA OA212 AIRFOIL Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file ONERA/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 (oa213il) ONERA OA213 AIRFOIL Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file ONERA/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 (oaf095il) OAF095 AIRFOIL Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file ONERA/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 (oaf102il) OAF102 AIRFOIL Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file ONERA/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 (oaf117il) OAF117 AIRFOIL Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file ONERA/Aerospatiale OAF117 Fenestron airfoil Max thickness 11.5% at 23.2% chord Max camber 2% at 46.9% chord Source UIUC Airfoil Coordinates Database (oaf128il) OAF128 AIRFOIL Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file ONERA/Aerospatiale OAF128 Fenestron airfoil Max thickness 12.8% at 23.2% chord Max camber 1% at 43.7% chord Source UIUC Airfoil Coordinates Database (oaf139il) OAF139 AIRFOIL Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file ONERA/Aerospatiale OAF139 Fenestron airfoil Max thickness 13.7% at 23.2% chord Max camber 0% at 0.1% chord Source UIUC Airfoil Coordinates Database Page 1 of 1

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  • 24/4/2015 Airfoildatabaselist(O)oa206iltooaf139il

    data:text/htmlcharset=utf8,%3Cbr%20class%3D%22Appleinterchangenewline%22%3E%3Ctable%20class%3D%22afSearchResult%22%20style%3D%22 1/1

    (oa206il)ONERAOA206AIRFOIL AirfoildetailsSendtoairfoilplotterAddtocomparisonLednicerformatdatfileSeligformatdatfileSourcedatfile

    ONERA/AerospatialeOA206rotorcraftairfoil(Constructedfrompatentandsmoothed)Maxthickness6%at31.8%chordMaxcamber0.8%at19.6%chordSourceUIUCAirfoilCoordinatesDatabase

    (oa209il)ONERAOA209AIRFOIL AirfoildetailsSendtoairfoilplotterAddtocomparisonLednicerformatdatfileSeligformatdatfileSourcedatfile

    ONERA/AerospatialeOA209rotorcraftairfoil(Constructedfrompatentandsmoothed)Maxthickness9%at29.3%chordMaxcamber1.6%at17.1%chordSourceUIUCAirfoilCoordinatesDatabase

    (oa212il)ONERAOA212AIRFOILAirfoildetailsSendtoairfoilplotterAddtocomparisonLednicerformatdatfileSeligformatdatfileSourcedatfile

    ONERA/AerospatialeOA212rotorcraftairfoil(Constructedfrompatentandsmoothed)Maxthickness12%at31.8%chordMaxcamber2.3%at31.8%chordSourceUIUCAirfoilCoordinatesDatabase

    (oa213il)ONERAOA213AIRFOILAirfoildetailsSendtoairfoilplotterAddtocomparisonLednicerformatdatfileSeligformatdatfileSourcedatfile

    ONERA/AerospatialeOA213rotorcraftairfoil(Constructedfrompatentandsmoothed)Maxthickness12.6%at32.5%chordMaxcamber3.3%at25%chordSourceUIUCAirfoilCoordinatesDatabase

    (oaf095il)OAF095AIRFOIL AirfoildetailsSendtoairfoilplotterAddtocomparisonLednicerformatdatfileSeligformatdatfileSourcedatfile

    ONERA/AerospatialeOAF095FenestronairfoilMaxthickness9.5%at23.2%chordMaxcamber3.9%at53.1%chordSourceUIUCAirfoilCoordinatesDatabase

    (oaf102il)OAF102AIRFOIL AirfoildetailsSendtoairfoilplotterAddtocomparisonLednicerformatdatfileSeligformatdatfileSourcedatfile

    ONERA/AerospatialeOAF102FenestronairfoilMaxthickness10.2%at28.7%chordMaxcamber3.6%at53.1%chordSourceUIUCAirfoilCoordinatesDatabase

    (oaf117il)OAF117AIRFOILAirfoildetailsSendtoairfoilplotterAddtocomparisonLednicerformatdatfileSeligformatdatfileSourcedatfile

    ONERA/AerospatialeOAF117FenestronairfoilMaxthickness11.5%at23.2%chordMaxcamber2%at46.9%chordSourceUIUCAirfoilCoordinatesDatabase

    (oaf128il)OAF128AIRFOILAirfoildetailsSendtoairfoilplotterAddtocomparisonLednicerformatdatfileSeligformatdatfileSourcedatfile

    ONERA/AerospatialeOAF128FenestronairfoilMaxthickness12.8%at23.2%chordMaxcamber1%at43.7%chordSourceUIUCAirfoilCoordinatesDatabase

    (oaf139il)OAF139AIRFOILAirfoildetailsSendtoairfoilplotterAddtocomparisonLednicerformatdatfileSeligformatdatfileSourcedatfile

    ONERA/AerospatialeOAF139FenestronairfoilMaxthickness13.7%at23.2%chordMaxcamber0%at0.1%chordSourceUIUCAirfoilCoordinatesDatabase

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