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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 /

Record Type:	Language materials, printed : Monograph/item
Title/Author:	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.
Reminder of title:	Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight /
remainder title:	Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight.
Author:	劉憲儒
Published:	雲林縣 :國立虎尾科技大學 , : 民113.01.,
Description:	[12], 64面 :圖, 表 ; : 30公分.;
Notes:	指導教授: 駱正穎.
Subject:	fluid structure interaction analysis. -
Online resource:	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:

1433939
fluid structure interaction analysis.

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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246 1 1 $a Analysis of Vibration Modal and Structural Forces of Composite Materials in Structures Tandem Wing UAV during Steady Flight.
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650 # 4 $a 流固耦合分析. $3 1000744
650 # 4 $a 模態分析. $3 998340
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