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串聯式雙翼無人機振動模態與穩態飛行中複材結構受力影響分析 = = Ana...

劉憲儒

串聯式雙翼無人機振動模態與穩態飛行中複材結構受力影響分析 = = Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight /

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	串聯式雙翼無人機振動模態與穩態飛行中複材結構受力影響分析 =/ 劉憲儒.
其他題名:	Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight /
其他題名:	Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight.
作者:	劉憲儒
出版者:	雲林縣 :國立虎尾科技大學 , : 民113.01.,
面頁冊數:	[12], 64面 :圖, 表 ; : 30公分.;
附註:	指導教授: 駱正穎.
標題:	串聯式雙翼無人機. -
電子資源:	電子資源

串聯式雙翼無人機振動模態與穩態飛行中複材結構受力影響分析 = = Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight /
劉憲儒

串聯式雙翼無人機振動模態與穩態飛行中複材結構受力影響分析 =Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight /Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight.劉憲儒. - 初版. - 雲林縣 :國立虎尾科技大學 ,民113.01. - [12], 64面 :圖, 表 ;30公分.

指導教授: 駱正穎.

碩士論文--國立虎尾科技大學飛機工程系航空與電子科技碩士班.

含參考書目.

(平裝).Subjects--Topical Terms:

1433937
串聯式雙翼無人機.

串聯式雙翼無人機振動模態與穩態飛行中複材結構受力影響分析 = = Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight /
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