[1]
H.S. Shen, J. Yang, Dynamic response of initially stressed functionally graded rectangular thin plates, Comp. struct. 54 (2001) 497-508.
DOI: 10.1016/s0263-8223(01)00122-2
Google Scholar
[2]
Y.W. Kim, Temperature dependent vibration analysis of functionally graded rectangular plates, J. of Sound and Vib. 284 (2005) 531-549.
DOI: 10.1016/j.jsv.2004.06.043
Google Scholar
[3]
A.A. Beni , P. Malekzadeh , Free vibration of functionally graded arbitrary straight sided quadrilateral plates in thermal environment. Comp. Struct. 92(2010) 2758-2767.
DOI: 10.1016/j.compstruct.2010.04.011
Google Scholar
[4]
B.M. Irons , The semiloof shell element, Proc. of the Conf. on finite elements for thin shell and curved members, London, (1976)pp.197-222.
Google Scholar
[5]
Monslin Sugirtha Singh, Kari Thangaratnam, Analysis of Functionally Graded plate and shells: Stress, Buckling and Vibration , J. of Aerospace Sciences and Technologies. 66, (2014) 127-136.
DOI: 10.4028/www.scientific.net/amr.984-985.402
Google Scholar
[6]
Palaninathan ,J. Ramachandran R.K. Thangaratnam , Thermal Buckling of Composite Laminated Plates. Comp Struct, 32(1989)1117-1124.
DOI: 10.1016/0045-7949(89)90413-6
Google Scholar
[7]
R. Dhanaraj, Palaninathan , Free vibration of initially stressed composite laminates, J. of. Sound and Vib. 142(1990) 365-378.
DOI: 10.1016/0022-460x(90)90656-k
Google Scholar
[8]
N. Virgin Lawrence, Vibration of Axially Loaded structures, Cambridge University press, (1990) pp.188-193.
Google Scholar
[9]
Ravikiren Kadoli ,N. Ganesan, Free vibration and buckling analysis of composite cylindrical shells conveying hot fluid, Comp Strut. 60 (2003)19-32.
DOI: 10.1016/s0263-8223(02)00313-6
Google Scholar
[10]
K.M. Liew, X Zhao, A mesh free method for analysis of the thermal and mechanical buckling of functionally graded cylindrical shell panels, Comput. Mech. 45(2010)297-310.
DOI: 10.1007/s00466-009-0446-8
Google Scholar
[11]
F.B. William, The vibration and buckling characteristics of cylindrical shells under axial load and external pressure. Technical Report. Airforce flight dynamics laboratory, Wright-Patterson Air Force Base, Ohio, (1967)AD65630.
DOI: 10.21236/ad0656302
Google Scholar