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
Link To Document :
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