Please use this identifier to cite or link to this item: http://hdl.handle.net/11455/2504
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dc.contributor.advisor郭正雄zh_TW
dc.contributor.advisorKuo Cheng Hsingen_US
dc.contributor.author林大祺zh_TW
dc.contributor.authorChi, Lin Taen_US
dc.date1994zh_TW
dc.date.accessioned2014-06-05T11:43:27Z-
dc.date.available2014-06-05T11:43:27Z-
dc.identifier.urihttp://hdl.handle.net/11455/2504-
dc.description.abstract本研究之實驗方式是利用步進馬達控制噴流條件而對三角翼翼面上方之渦 漩結構作擾動. 結果顯示:注入噴流動量愈大, 能延遲渦漩之潰散. 渦漩 潰散位置經擾動後之回復速度大致保持一定. 攻角愈大, 其回復速度愈 大. 此回復速度與噴 動量大小無關. 對於較小之後掠角(60度)經擾動後 之回復過程中會有渦漩潰散位置停留及徘徊的現象, 而在高後掠角 (75度)時則未曾發現. 此現象實與翼面上方渦漩結構之發展行為有很大的 關係.zh_TW
dc.language.isoen_USzh_TW
dc.publisher機械工程研究所zh_TW
dc.subjectblowing perturbationen_US
dc.subject噴流擾動zh_TW
dc.subjectrecover speeden_US
dc.subject回復速度zh_TW
dc.title三角翼上方渦漩結構受噴流擾動之暫態特性研究zh_TW
dc.titleStudy of The Transient Vortical Structure Over Delta Wing Subjected to Blowing Perturbationsen_US
dc.typeThesis and Dissertationzh_TW
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.openairetypeThesis and Dissertation-
item.cerifentitytypePublications-
item.fulltextno fulltext-
item.languageiso639-1en_US-
item.grantfulltextnone-
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