DocumentCode
496282
Title
Optimization Design of the Supporting Stiffness of T-tail
Author
Qiu, Ju ; Sun, Qin
Author_Institution
Sch. of Aeronaut., Northwestern Polytech. Univ., Xi´´an, China
Volume
1
fYear
2009
fDate
24-26 April 2009
Firstpage
279
Lastpage
282
Abstract
In this paper, the dynamic model of T-tail is introduced, and the relationship among the natural frequency, the supporting stiffness, the supporting point position and the flutter velocity is analyzed through the optimization process. The optimization for minimum weight, the supporting stiffness and the supporting point shift for optimization variations, and the flutter speed and the natural frequency for optimization constraints. Lastly, we plot two variable curves (support stiffness VS. flutter speed, Flutter velocity variation VS. Z coordinate Variation), and draw a conclusion that the stiffness and supporting position variations can be more beneficial to enhance the flutter velocity.
Keywords
aircraft control; controllers; optimisation; position control; velocity control; T-tail configuration; flutter speed; flutter velocity; optimization process; velocity stiffness; Aerodynamics; Aerospace engineering; Aircraft; Constraint optimization; Design optimization; Elevators; Frequency; Sensitivity analysis; Sun; Tail; T-tail; flutter speed; optimization; supporting stiffness;
fLanguage
English
Publisher
ieee
Conference_Titel
Computational Sciences and Optimization, 2009. CSO 2009. International Joint Conference on
Conference_Location
Sanya, Hainan
Print_ISBN
978-0-7695-3605-7
Type
conf
DOI
10.1109/CSO.2009.42
Filename
5193694
Link To Document