Nonlinear Vibrations of FGM Circular Conical Panel Under In-Plane and Transverse Excitation
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Publisher
Springer Science and Business Media LLC
Link
http://link.springer.com/article/10.1007/s42417-018-0063-y/fulltext.html
Reference27 articles.
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3. Teichmann D (1985) An approximation of the lowest eigen frequencies and buckling loads of cylindrical and conical shell panels under initial stress. AIAA J 23:1634–1637
4. Qiu WB, Zhou ZH, Xu XS (2016) The dynamic behavior of circular plates under impact loads. J Vib Eng Technol 4:111–116
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