DocumentCode :
3031211
Title :
A method for indirect measurement of vibration stress of thin cylindrical shell
Author :
Hui Li ; Jingyu Zhai ; Dejun Pan ; Qingkai Han
Author_Institution :
Sch. of Mech. Eng. & Autom., Northeastern Univ., Shenyang, China
fYear :
2013
fDate :
20-22 Dec. 2013
Firstpage :
3673
Lastpage :
3677
Abstract :
A method for indirect measurement of vibration stress of thin cylindrical shell (TCS) was proposed in this study. Firstly, TCS´s vibration stress and response under different base excitation amplitudes were calculated by harmonic response analysis method. Subsequently the relationship between the vibration stress and response of TCS was established, so that indirect measurement principle of vibration stress was clarified. Secondly, the procedure of indirectly measuring TCS´s vibration stress was proposed, and its key steps, such as the determination of Rayleigh damping and modification of finite element model of TCS through the experimental results were explained in details. Finally, practicability and accuracy of this indirect method was demonstrated by a study case. The results showed that indirect measurement results of vibration stress had good agreements with actual experimental results, which can provide a new idea for obtaining TCS´s vibration stress.
Keywords :
damping; finite element analysis; shells (structures); structural engineering; vibration measurement; Rayleigh damping; TCS; base excitation amplitudes; finite element model; harmonic response analysis method; indirect measurement; thin cylindrical shell; vibration response; vibration stress; Damping; Frequency measurement; Strain; Stress; Stress measurement; Vibration measurement; Vibrations; indirect measurement; thin cylindrical shell; vibration response; vibration stress;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronic Sciences, Electric Engineering and Computer (MEC), Proceedings 2013 International Conference on
Conference_Location :
Shengyang
Print_ISBN :
978-1-4799-2564-3
Type :
conf
DOI :
10.1109/MEC.2013.6885635
Filename :
6885635
Link To Document :
بازگشت