@inproceedings{3bd1e9d176bc4c2aa7726375dd518966,
title = "Study on random vibration response analysis for the sphere cylinder assembly in aerospace vehicle",
abstract = "To assess the structural strength of spherical cylinder, the finite element model was constructed by the NX NASTRAN software. Firstly, the basic principle of random vibration response analysis was introduced, then the random vibration response analysis of the cylinder assembly was analyzed. The simulation result shows that the stress of the joint between spherical cylinder clamp and the base is larger than other areas in conditions of a given random vibration load. The spherical cylinder structure is safe and that the maximum RMS stress is about 20 MPa.",
keywords = "Modal, Random vibration, Spherical cylinder clamp, The power spectral density function",
author = "Sun, {De Lin} and Zhe Zhao and Kun He and Liao, {Ri Dong}",
note = "Publisher Copyright: {\textcopyright} (2014) Trans Tech Publications, Switzerland.; 2nd International Conference on Mechanical Structures and Smart Materials, 2nd ICMSSM 2014 ; Conference date: 16-08-2014 Through 17-08-2014",
year = "2014",
doi = "10.4028/www.scientific.net/AMM.680.258",
language = "English",
series = "Applied Mechanics and Materials",
publisher = "Trans Tech Publications Ltd.",
pages = "258--262",
editor = "Salmah Husseinsyah and Salmah Husseinsyah",
booktitle = "Materials Science, Mechanical Structures and Engineering",
address = "Switzerland",
}