• 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