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Low-Speed Stability and Control of E...

Langston, Sarah.

Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations.

紀錄類型:	書目-語言資料,手稿 : Monograph/item
正題名/作者:	Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations./
作者:	Langston, Sarah.
面頁冊數:	1 online resource (102 pages)
附註:	Source: Masters Abstracts International, Volume: 55-02.
Contained By:	Masters Abstracts International55-02(E).
標題:	Aerospace engineering. -
電子資源:	click for full text (PQDT)
ISBN:	9781339072579

Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations.
Langston, Sarah.

Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations. - 1 online resource (102 pages)

Source: Masters Abstracts International, Volume: 55-02.

Thesis (Master's)

Includes bibliographical references

This thesis presents studies of the low-speed stability and control of a representative long-range supersonic flight vehicle. The aircraft of interest is a research uninhabited aerial vehicle (R-UAV), a 1/16th scaled model of a concept supersonic business jet. Evaluation of stability and control characteristics is based on a linear time-invariant state-space small-perturbations approach. Low-speed wind tunnel results together with unsteady aerodynamic panel method analysis are the basis for the aerodynamic stability derivatives used. The main goal of this work is to study the effects on stability and controllability of reduction in size or complete elimination of tail surfaces, with particular emphasis on the vertical tail.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2018

Mode of access: World Wide Web

ISBN: 9781339072579Subjects--Topical Terms:

686400
Aerospace engineering.
Index Terms--Genre/Form:

554714
Electronic books.

Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations.
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035 $a AAI1599847
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100 1 $a Langston, Sarah. $3 1180417
245 1 0 $a Low-Speed Stability and Control of Exploratory Tailless Long-Range Supersonic Configurations.
264 0 $c 2015
300 $a 1 online resource (102 pages)
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
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500 $a Source: Masters Abstracts International, Volume: 55-02.
500 $a Adviser: Eli Livne.
502 $a Thesis (Master's) $c University of Washington $d 2015.
504 $a Includes bibliographical references
520 $a This thesis presents studies of the low-speed stability and control of a representative long-range supersonic flight vehicle. The aircraft of interest is a research uninhabited aerial vehicle (R-UAV), a 1/16th scaled model of a concept supersonic business jet. Evaluation of stability and control characteristics is based on a linear time-invariant state-space small-perturbations approach. Low-speed wind tunnel results together with unsteady aerodynamic panel method analysis are the basis for the aerodynamic stability derivatives used. The main goal of this work is to study the effects on stability and controllability of reduction in size or complete elimination of tail surfaces, with particular emphasis on the vertical tail.
533 $a Electronic reproduction. $b Ann Arbor, Mich. : $c ProQuest, $d 2018
538 $a Mode of access: World Wide Web
650 4 $a Aerospace engineering. $3 686400
655 7 $a Electronic books. $2 local $3 554714
690 $a 0538
710 2 $a ProQuest Information and Learning Co. $3 1178819
710 2 $a University of Washington. $b Aeronautics and Astronautics. $3 1178958
773 0 $t Masters Abstracts International $g 55-02(E).
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1599847 $z click for full text (PQDT)

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