2008
DOI: 10.1016/j.jsv.2008.03.056
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Free vibration analysis of functionally graded curved panels using a higher-order finite element formulation

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Cited by 210 publications
(91 citation statements)
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“…It may be concluded that the present results exhibit close range with the above cited reference data for the maximum number of cases. Maximum exception cases in first frequency mode are observed with Pradyumna and Bandyopadhyay [17] for the values of power law exponent n = 0.0, 2.0 and 10.0. The probable reason may be due to the different model of higher order theory involved in the reference paper by Pradyumna and Bandyopadhyay [17].…”
Section: Free Vibration Analysis-validation Studymentioning
confidence: 89%
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“…It may be concluded that the present results exhibit close range with the above cited reference data for the maximum number of cases. Maximum exception cases in first frequency mode are observed with Pradyumna and Bandyopadhyay [17] for the values of power law exponent n = 0.0, 2.0 and 10.0. The probable reason may be due to the different model of higher order theory involved in the reference paper by Pradyumna and Bandyopadhyay [17].…”
Section: Free Vibration Analysis-validation Studymentioning
confidence: 89%
“…{q}appearing in Equation (12) is the dynamic pressure applied on the top of the shell. It is given by, q x, y,t ( ) = q 0 F(t) (17) Here, q 0 is the maximum amplitude and F(t)is a dynamic load shape function of time domain. In the present analysis F(t) is taken as unity for the case of suddenly applied load.…”
Section: Dynamic Responsementioning
confidence: 99%
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“…This is especially true for linear problems (Lam et al (2002); Loy et al (2008); Matsunaga (2008); Neves et al (2013); Pradyumna and Bandyopadhyay (2008); Reddy et al (1999); Reddy (2009);Shen (2009) ;Viola (2007, 2009) ;Tornabene et al (2011);Zhu et al (2014Zhu et al ( , 2015). However, in the last decade, nonlinear free and forced vibrations of the FG shells have been extensively studied as well (Reddy et al (1999); Reddy (2009);Shen (2009); Amabili (2008); Alijani et al (2011a,b); Bich et al (2012); Chorfi and Houmat (2010); Sundararajan et al (2005); Woo et al (2006); Xiang et al (2015); Zhao and Liew (2009)).…”
Section: Introductionmentioning
confidence: 99%
“…Pradyumna S. and Bandyspadhyay J.N. received natural frequencies of FGM curved panels using highorder finite element formulation [5]. Pradhan S.C et al [6] and Loy C.T et al [7] studied vibration of FGM cylindrical shells and the effects of boundary conditions and power law indices on the natural frequencies of shells; Yang Y. and Shen H.S.…”
Section: Introductionmentioning
confidence: 99%