{"@context":{"@vocab":"https://cir.nii.ac.jp/schema/1.0/","rdfs":"http://www.w3.org/2000/01/rdf-schema#","dc":"http://purl.org/dc/elements/1.1/","dcterms":"http://purl.org/dc/terms/","foaf":"http://xmlns.com/foaf/0.1/","prism":"http://prismstandard.org/namespaces/basic/2.0/","cinii":"http://ci.nii.ac.jp/ns/1.0/","datacite":"https://schema.datacite.org/meta/kernel-4/","ndl":"http://ndl.go.jp/dcndl/terms/","jpcoar":"https://github.com/JPCOAR/schema/blob/master/2.0/"},"@id":"https://cir.nii.ac.jp/crid/1390564227299718656.json","@type":"Article","productIdentifier":[{"identifier":{"@type":"DOI","@value":"10.2322/tjsass.62.247"}},{"identifier":{"@type":"URI","@value":"https://www.jstage.jst.go.jp/article/tjsass/62/5/62_T-17-98/_pdf"}},{"identifier":{"@type":"NAID","@value":"130007702001"}}],"dc:title":[{"@language":"en","@value":"Development of Engineering Model Providing Body Force Distribution of Tri-Electrode Plasma Actuator"}],"dc:language":"en","description":[{"type":"abstract","notation":[{"@language":"en","@value":"<p>Tri-electrode plasma actuators (TED-PAs) can induce a stronger jet than that of conventional two-electrode plasma actuators (DBDPAs). For practical application of a TED-PA, it is significant to develop a TED-PA engineering model for implementing CFD simulations. In this study, we model the body force distribution generated by a TED-PA utilizing the Suzen model, which is one of engineering models used for DBDPAs. First, we define a function to describe the charge distribution profile on the dielectric surface with two half-Gaussian distributions. Second, we define the maximum values of surface charge as functions of the voltage applied based on the plasma simulation results. Finally, the flow fields numerically obtained using the model developed are compared with the experimental results from our previous study. Although there are some discrepancies mainly due to the two-dimensional laminar flow simulation, the model developed can quantitatively reproduce the voltage characteristics of thrust force and the jet structure induced. Therefore, the model developed is expected to evaluate the flow control effect precisely.</p>"}],"abstractLicenseFlag":"disallow"}],"creator":[{"@id":"https://cir.nii.ac.jp/crid/1410564227299718658","@type":"Researcher","personIdentifier":[{"@type":"NRID","@value":"9000404106064"}],"foaf:name":[{"@language":"en","@value":"TANAKA Yuhi"}],"jpcoar:affiliationName":[{"@language":"en","@value":"Research Laboratory, IHI Corporation"}]},{"@id":"https://cir.nii.ac.jp/crid/1420282801213918208","@type":"Researcher","personIdentifier":[{"@type":"KAKEN_RESEARCHERS","@value":"90432608"},{"@type":"NRID","@value":"1000090432608"},{"@type":"NRID","@value":"9000017329325"},{"@type":"NRID","@value":"9000006675054"},{"@type":"NRID","@value":"9000408815137"},{"@type":"NRID","@value":"9000408815144"},{"@type":"NRID","@value":"9000410884682"},{"@type":"NRID","@value":"9000308050109"},{"@type":"NRID","@value":"9000410655994"},{"@type":"NRID","@value":"9000398791607"},{"@type":"NRID","@value":"9000240083380"},{"@type":"NRID","@value":"9000345405003"},{"@type":"NRID","@value":"9000240061767"},{"@type":"NRID","@value":"9000020915317"},{"@type":"NRID","@value":"9000404106065"},{"@type":"NRID","@value":"9000402373821"},{"@type":"NRID","@value":"9000265252055"},{"@type":"RESEARCHMAP","@value":"https://researchmap.jp/tmtn"}],"foaf:name":[{"@language":"en","@value":"MATSUNO Takashi"}],"jpcoar:affiliationName":[{"@language":"en","@value":"Department of Mechanical and Aerospace Engineering, Tottori University"}]},{"@id":"https://cir.nii.ac.jp/crid/1410564227299718657","@type":"Researcher","personIdentifier":[{"@type":"NRID","@value":"9000404106063"}],"foaf:name":[{"@language":"en","@value":"ASAUMI Norio"}],"jpcoar:affiliationName":[{"@language":"en","@value":"Research Laboratory, IHI 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Hiroyuki"}],"jpcoar:affiliationName":[{"@language":"en","@value":"Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology"}]},{"@id":"https://cir.nii.ac.jp/crid/1420004222329774208","@type":"Researcher","personIdentifier":[{"@type":"KAKEN_RESEARCHERS","@value":"20897813"},{"@type":"NRID","@value":"1000020897813"},{"@type":"NRID","@value":"9000410655992"},{"@type":"NRID","@value":"9000398791610"},{"@type":"NRID","@value":"9000368924731"},{"@type":"NRID","@value":"9000412551984"},{"@type":"NRID","@value":"9000404106061"},{"@type":"NRID","@value":"9000411484937"},{"@type":"NRID","@value":"9000414521952"},{"@type":"RESEARCHMAP","@value":"https://researchmap.jp/kumi_nakai"}],"foaf:name":[{"@language":"en","@value":"NAKAI Kumi"}],"jpcoar:affiliationName":[{"@language":"en","@value":"Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology"}]}],"publication":{"publicationIdentifier":[{"@type":"PISSN","@value":"05493811"},{"@type":"LISSN","@value":"05493811"},{"@type":"EISSN","@value":"21894205"}],"prism:publicationName":[{"@language":"en","@value":"TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES"},{"@language":"en","@value":"Trans. Japan Soc. Aero. S Sci."}],"dc:publisher":[{"@language":"en","@value":"THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES"},{"@language":"ja","@value":"一般社団法人 日本航空宇宙学会"}],"prism:publicationDate":"2019","prism:volume":"62","prism:number":"5","prism:startingPage":"247","prism:endingPage":"255"},"reviewed":"false","dcterms:accessRights":"http://purl.org/coar/access_right/c_abf2","url":[{"@id":"https://www.jstage.jst.go.jp/article/tjsass/62/5/62_T-17-98/_pdf"}],"availableAt":"2019","foaf:topic":[{"@id":"https://cir.nii.ac.jp/all?q=Plasma%20Actuator","dc:title":"Plasma Actuator"},{"@id":"https://cir.nii.ac.jp/all?q=Body%20Force","dc:title":"Body Force"},{"@id":"https://cir.nii.ac.jp/all?q=Engineering%20Model","dc:title":"Engineering Model"},{"@id":"https://cir.nii.ac.jp/all?q=Computational%20Fluid%20Dynamics","dc:title":"Computational Fluid Dynamics"}],"relatedProduct":[{"@id":"https://cir.nii.ac.jp/crid/1360292619156910208","@type":"Article","relationType":["references"],"jpcoar:relatedTitle":[{"@value":"Numerical Simulations of Flow Separation Control in Low-Pressure Turbines Using Plasma Actuators"}]},{"@id":"https://cir.nii.ac.jp/crid/1360567184877662336","@type":"Article","resourceType":"学術雑誌論文(journal article)","relationType":["references"],"jpcoar:relatedTitle":[{"@value":"High-performance computing-based exploration of flow control with micro devices"}]},{"@id":"https://cir.nii.ac.jp/crid/1360572092661462528","@type":"Article","resourceType":"学術雑誌論文(journal article)","relationType":["isReferencedBy"],"jpcoar:relatedTitle":[{"@value":"Validity of Three-Fluid Plasma Modeling for Alternating-Current Dielectric-Barrier-Discharge Plasma Actuator"}]},{"@id":"https://cir.nii.ac.jp/crid/1360574094912537728","@type":"Article","relationType":["references"],"jpcoar:relatedTitle":[{"@value":"Validation Study of Numerical 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