Estimation of the Lift-to-Drag Ratio Using the Lifting Line Method: Application to a Leading Edge Inflatable Kite
The use of kites for auxiliary propulsion reduces oil consumption for vessels. But the complexity of the kite numerical simulation induces the development of computationally efficient models based on lifting line theory to evaluate the aerodynamic characteristics of the kite. The presented 3D liftin...
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| creator | Parlier, Yves Roncin, Kostia Bles, Guilhem Jochum, Christian Leroux, Jean-Baptiste Leloup, Richard |
| description | The use of kites for auxiliary propulsion reduces oil consumption for vessels. But the complexity of the kite numerical simulation induces the development of computationally efficient models based on lifting line theory to evaluate the aerodynamic characteristics of the kite. The presented 3D lifting line model takes into account the three-dimensional shape of the kite and the viscosity of the fluid. The proposed model was applied to a F-one Revolt Leading Edge Inflatable kite to predict its lift-to-drag ratio. Finally, this method is in very good agreement with CFD simulations in the case of a paragliding wing, but needs a much smaller computational effort. |
| doi_str_mv | 10.1007/978-3-642-39965-7_19 |
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Finally, this method is in very good agreement with CFD simulations in the case of a paragliding wing, but needs a much smaller computational effort.</description><subject>Aerodynamic Characteristic</subject><subject>Aerodynamics</subject><subject>Alternative & renewable energy sources & technology</subject><subject>Collocation Point</subject><subject>Dynamical Systems</subject><subject>ENERGY TECHNOLOGY & ENGINEERING</subject><subject>Engineering Sciences</subject><subject>Fluid mechanics</subject><subject>Fluids mechanics</subject><subject>Horseshoe Vortex</subject><subject>Lift Line</subject><subject>Lift Line Theory</subject><subject>Mathematics</subject><subject>Mechanics</subject><subject>Physics</subject><subject>Solid mechanics</subject><issn>1865-3529</issn><issn>1865-3537</issn><isbn>9783642399640</isbn><isbn>3642399649</isbn><isbn>9783642399657</isbn><isbn>3642399657</isbn><isbn>9783642399657</isbn><isbn>3642399657</isbn><fulltext>true</fulltext><rsrctype>book_chapter</rsrctype><creationdate>2013</creationdate><recordtype>book_chapter</recordtype><recordid>eNpVUctO3DAUdSlFHcH8QNWFt1249St23N2ITgsiCKkqa8txrjMpIQ6Ji8Tf45AKiZWt87LvuQh9ZvQro1R_M7okgijJiTBGFURbZt6hbYZFBl8wfYQ2rMycKIR-_4aT9PiV4-YEbUrFqSyNFB_Rdp7_UkoZlUYUbIMe9nPq7l3q4oBjwOkAuOpCIimSH5Nr8e-FwrdzN7Sv5HKvugHwNaRDbL7j3Tj2nV9DUsQOV-CaRbVvWsCXQ-hdcnUP-KpLcIY-BNfPsP1_nqLbn_s_5xekuvl1eb6rSMuNSiQUHrwLDITXILVqVG0axh0vjfeqVqqReQjmtdamLOpAnTYqNME03NdccHGKvqy5B9fbccpDTk82us5e7Cq7YJQaqmnJH1nW8lU7Z-HQwmTrGO9my6hd9mFzuVbYXK996d4u-8gmuZrGKT78gzlZWFwehjS53h_cmGDKGVIpobKjkFZIlW2fVlvrerCPU2-VYiI_Q_OnnwFaOI-9</recordid><startdate>2013</startdate><enddate>2013</enddate><creator>Parlier, Yves</creator><creator>Roncin, Kostia</creator><creator>Bles, Guilhem</creator><creator>Jochum, Christian</creator><creator>Leroux, Jean-Baptiste</creator><creator>Leloup, Richard</creator><general>Springer Berlin / Heidelberg</general><general>Springer Berlin Heidelberg</general><general>Springer</general><scope>FFUUA</scope><scope>1XC</scope><orcidid>https://orcid.org/0000-0002-3244-5181</orcidid><orcidid>https://orcid.org/0000-0001-7083-8149</orcidid></search><sort><creationdate>2013</creationdate><title>Estimation of the Lift-to-Drag Ratio Using the Lifting Line Method: Application to a Leading Edge Inflatable Kite</title><author>Parlier, Yves ; Roncin, Kostia ; Bles, Guilhem ; Jochum, Christian ; Leroux, Jean-Baptiste ; Leloup, Richard</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-g296t-f5cecaf1e3c7e476d6b9d12a289cc6b66d41041c777985bf0a796fdf9d2cb2323</frbrgroupid><rsrctype>book_chapters</rsrctype><prefilter>book_chapters</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Aerodynamic Characteristic</topic><topic>Aerodynamics</topic><topic>Alternative & renewable energy sources & technology</topic><topic>Collocation Point</topic><topic>Dynamical Systems</topic><topic>ENERGY TECHNOLOGY & ENGINEERING</topic><topic>Engineering Sciences</topic><topic>Fluid mechanics</topic><topic>Fluids mechanics</topic><topic>Horseshoe Vortex</topic><topic>Lift Line</topic><topic>Lift Line Theory</topic><topic>Mathematics</topic><topic>Mechanics</topic><topic>Physics</topic><topic>Solid mechanics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Parlier, Yves</creatorcontrib><creatorcontrib>Roncin, Kostia</creatorcontrib><creatorcontrib>Bles, Guilhem</creatorcontrib><creatorcontrib>Jochum, Christian</creatorcontrib><creatorcontrib>Leroux, Jean-Baptiste</creatorcontrib><creatorcontrib>Leloup, Richard</creatorcontrib><collection>ProQuest Ebook Central - Book Chapters - Demo use only</collection><collection>Hyper Article en Ligne (HAL)</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Parlier, Yves</au><au>Roncin, Kostia</au><au>Bles, Guilhem</au><au>Jochum, Christian</au><au>Leroux, Jean-Baptiste</au><au>Leloup, Richard</au><au>Diehl, Moritz</au><au>Schmehl, Roland</au><au>Ahrens, Uwe</au><au>Schmehl, Roland</au><au>Ahrens, Uwe</au><au>Diehl, Moritz</au><format>book</format><genre>bookitem</genre><ristype>CHAP</ristype><atitle>Estimation of the Lift-to-Drag Ratio Using the Lifting Line Method: Application to a Leading Edge Inflatable Kite</atitle><btitle>Airborne Wind Energy</btitle><seriestitle>Green Energy and Technology</seriestitle><date>2013</date><risdate>2013</risdate><spage>339</spage><epage>355</epage><pages>339-355</pages><issn>1865-3529</issn><eissn>1865-3537</eissn><isbn>9783642399640</isbn><isbn>3642399649</isbn><isbn>9783642399657</isbn><isbn>3642399657</isbn><eisbn>9783642399657</eisbn><eisbn>3642399657</eisbn><abstract>The use of kites for auxiliary propulsion reduces oil consumption for vessels. 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| identifier | ISSN: 1865-3529 |
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| language | eng |
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| source | Springer Books; Alma/SFX Local Collection |
| subjects | Aerodynamic Characteristic Aerodynamics Alternative & renewable energy sources & technology Collocation Point Dynamical Systems ENERGY TECHNOLOGY & ENGINEERING Engineering Sciences Fluid mechanics Fluids mechanics Horseshoe Vortex Lift Line Lift Line Theory Mathematics Mechanics Physics Solid mechanics |
| title | Estimation of the Lift-to-Drag Ratio Using the Lifting Line Method: Application to a Leading Edge Inflatable Kite |
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