• DocumentCode
    691312
  • Title

    Thermal response analysis of variable stiffness of piezoelectric cylindrical shell

  • Author

    Lei Wang ; Hong-hao Yue ; Jing Jiang ; Wen-yuan Li ; Xu Hou

  • Author_Institution
    Sch. of Naval Archit. & Ocean Eng., Harbin Inst. of Technol. at Weihai, Weihai, China
  • fYear
    2013
  • fDate
    25-27 Oct. 2013
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    Materials and structures been unpredictable changed by sudden changes in temperature, alternation temperature and local temperature. The temperature change in structures´ surface may coursed by air friction or sunlight illumination in the aerospace environment. In this paper, modal analysis of cylindrical shell by ANSYS is proposed. Static force which been saw as the PZT patches´ acting force is added to the cylindrical shell´s internal surface. The frequency will be changed by the aeroheating environment and the force. And in this paper, a method to adding force to restore the frequency is proposed.
  • Keywords
    elastic constants; piezoelectricity; shells (structures); thermal analysis; PZT patche; aeroheating environment; aerospace environment; air friction; cylindrical shell internal surface; piezoelectric cylindrical shell; static force; sunlight illumination; thermal response analysis; Integrated circuits; Ansys; Cylindrical shell; Pzt; Temperature field;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Piezoelectricity, Acoustic Waves and Device Applications (SPAWDA), 2013 Symposium on
  • Conference_Location
    Changsha
  • Print_ISBN
    978-1-4799-3289-4
  • Type

    conf

  • DOI
    10.1109/SPAWDA.2013.6841099
  • Filename
    6841099