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Membrane and adaptively-shaped wings...

Lian, Yongsheng.

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Membrane and adaptively-shaped wings for micro air vehicles.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Membrane and adaptively-shaped wings for micro air vehicles./
作者:	Lian, Yongsheng.
面頁冊數:	126 p.
附註:	Source: Dissertation Abstracts International, Volume: 65-01, Section: B, page: 0301.
Contained By:	Dissertation Abstracts International65-01B.
標題:	Engineering, Aerospace. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3120132
ISBN:	0496675044

Membrane and adaptively-shaped wings for micro air vehicles.
Lian, Yongsheng.

Membrane and adaptively-shaped wings for micro air vehicles. - 126 p.

Source: Dissertation Abstracts International, Volume: 65-01, Section: B, page: 0301.

Thesis (Ph.D.)--University of Florida, 2003.

Micro air vehicles (MAVs), with wing span of 15 cm or less and flight speed around 10 m/s, have many applications in both civilian and military areas. The Reynolds number based on the given parameters is around 10 4, which often yields insuffici

ISBN: 0496675044Subjects--Topical Terms:

1018395
Engineering, Aerospace.

Membrane and adaptively-shaped wings for micro air vehicles.
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245 1 0 $a Membrane and adaptively-shaped wings for micro air vehicles.
300 $a 126 p.
500 $a Source: Dissertation Abstracts International, Volume: 65-01, Section: B, page: 0301.
500 $a Chair: Wei Shyy.
502 $a Thesis (Ph.D.)--University of Florida, 2003.
520 $a Micro air vehicles (MAVs), with wing span of 15 cm or less and flight speed around 10 m/s, have many applications in both civilian and military areas. The Reynolds number based on the given parameters is around 10 4, which often yields insuffici
520 $a The present study focuses on developing computational and modeling capabilities to better understand the MAV aerodynamics. Both flexible wings, utilizing membrane materials, and adaptively-shaped wings, utilizing piezo-actuated flaps, have been
520 $a Besides the aerodynamic study, we also perform shape optimization to improve the membrane wing performance. Since direct optimization of a membrane wing is too time consuming to be practical, we optimize a surrogate rigid wing model based on an
590 $a School code: 0070.
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650 4 $a Applied Mechanics. $3 1018410
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710 2 0 $a University of Florida. $3 718949
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