1 |
Abbas, L.K., Rui, X., Marzocca, P., Abdalla, M. and De Breuker, R. (2011), "A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel", Acta Mech., 222, 41-57.
DOI
|
2 |
Armenakas, A.E., Gazis, D.C. and Herrmann, G. (1969), Free Vibrations of Circular Cylindrical Shells, Oxford, Pergamon Press.
|
3 |
Biglari, H. and Jafari, A.A. (2010), "Static and free vibration analyses of doubly curved composite sandwich panels with soft core based on a new three-layered mixed theory", Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci., 224, 2332-2349.
DOI
|
4 |
Fekrar., A., El Meiche, N., Bessaim, A., Tounsi, A. and Adda Bedia, E.A. (2012), "Buckling analysis of functionally graded hybrid composite plates using a new four variable refined plate theory", Steel Comp. Struct., 13(1), 91-107.
DOI
|
5 |
Frostig, Y. and Baruch, M. (1994), "Free vibration of sandwich beams with a transversely flexible core: a high order approach", J. Sound Vib., 176(2), 195-208.
DOI
|
6 |
Frostig, Y. and Thomsen, O.T. (2004), "Higher-order free vibration of sandwich panels with a flexible core", Int. J. Solid. Struct., 41, 1697-1724.
DOI
|
7 |
Ganapathi, M. and Varadan, T.K. (1995), "Supersonic Flutter of laminated curved panels", Defence Sci. J., 45(2), 147-159.
DOI
|
8 |
Jalili, S., Zamani, J., Shariyat, M., Jalili, N., Ajdari, M.A.B. and Jafari, M. (2014), "Experimental and numerical investigation of composite conical shells", Struct. Eng. Mech., 49(5), 555-568.
DOI
|
9 |
Kheirikhah, M.M., Khalili, S.M.R. and Malekzadeh Fard, K. (2012), "Analytical solution for bending analysis of soft-core composite sandwich plates using improved high-order theory", Struct. Eng. Mech., 44(1), 15-34.
DOI
|
10 |
Kuo, S.Y. (2011), "Flutter of rectangular composite plates with variable fiber pacing", Comp. Struct., 93, 2533-2540.
DOI
|
11 |
Leissa, A.W. and Kadi, A.S. (1971), "Curvature effects on shallow shell vibrations", J. Sound Vib., 16(2), 173-187.
DOI
|
12 |
Li, F.M. and Song, Z.G. (2013), "Flutter and thermal buckling control for composite laminated panels in supersonic flow", J. Sound Vib., 332, 5678-5695.
DOI
|
13 |
Malekzadefard, K., Livani, M. and Ashena Ghasemi, F. (2014a), "Improved high order free vibration analysis of thick double curved sandwich panels with transversely flexible cores", Lat. Am. J. Solid. Struct., 11, 2284-2307.
DOI
|
14 |
Malekzadefard, K., Livani, M., Veisi, A. and Gholami, M. (2014b), "Improved high-order bending analysis of double curved sandwich panels subjected to multiple loading conditions", Lat. Am. J. Solid. Struct., 11, 1591-1614.
DOI
|
15 |
Malekzadeh Fard, K. and Livani, M. (2015), "The buckling of truncated conical sandwich panels under axial compression and external pressure", Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci., 229(11), 1965-1978.
DOI
|
16 |
Meunier, M. and Shenoi, R.A. (1999), "Free vibration analysis of composite sandwich plates", Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci., 213(7), 715-727.
DOI
|
17 |
Moradi, S. and Mansouri, M.H. (2012), "Thermal buckling analysis of shear deformable laminated orthotropic plates by differential quadrature", Steel Compos. Struct., 12(2), 129-147.
DOI
|
18 |
Naj, R., Sabzikar Boroujerdy, M. and Eslami, M.R. (2008), "Thermal and mechanical instability of functionally graded truncated conical shells", Thin Wall. Struct., 46(1), 65-78.
DOI
|
19 |
Navazi, H.M. and Haddadpour, H. (2007), "Aero-thermoelastic stability of functionally graded plates", Compos. Struct., 80, 580-587.
DOI
|
20 |
Navazi, H.M. and Haddadpour, H. (2011), "Nonlinear aero-thermoelastic analysis of homogeneous and functionally graded plates in supersonic airflow using coupled models", Compos. Struct., 93, 2554-2565.
DOI
|
21 |
Nguyen, T.K., Thai, H.T. and Vo, P.T. (2015), "A refined higher-order shear deformation theory for bending, vibration and buckling analysis of functionally graded sandwich plates", Steel Compos. Struct., 18(1), 91-120.
DOI
|
22 |
Nguyen, T.K., Vo, P.T. and Thai, H.T. (2014a), "Vibration and buckling analysis of functionally graded sandwich plates with improved transverse shear stiffness based on the first-order shear deformation theory", Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci., 228(12), 2110-2131.
DOI
|
23 |
Nguyen, V.H., Nguyen, T.K., Thai, H.T. and Vo, T.P. (2014b), "A new inverse trigonometric shear deformation theory for isotropic and functionally graded sandwich plates", Compos. Part B: Eng., 66, 233-246.
DOI
|
24 |
Rahmani, O., Khalili, S.M.R. and Malekzadeh, K. (2009), "Free vibration response of composite sandwich cylindrical shell with flexible core", Compos. Struct., 92, 1269-1281.
|
25 |
Rahmani, O., Khalili, S.M.R. and Malekzadeh, K. (2010), "Free vibration response of composite sandwich cylindrical shell with flexible core", Compos. Struct., 92, 1269-1281.
DOI
|
26 |
Reddy, J.N. (2004), Mechanics of Laminated Composite Plates and Shells, Theory and Analysis. CRC Press, New York, USA.
|
27 |
Rezaiee-Pajand, M., Shahabian, F. and Tavakoli, F.H. (2012), "A new higher-order triangular plate bending element for the analysis of laminated composite and sandwich plates", Struct. Eng. Mech., 43(2), 253-271.
DOI
|
28 |
Sawyer, J.W. (1977), "Flutter and buckling of general laminated plates", J. Aircraft, 14, 387-393.
DOI
|
29 |
Sankar, A., Natarajan, S., Ben Zineb, T. and Ganapathi, M. (2015), "Investigation of supersonic flutter of thick doubly curved sandwich panels with CNT reinforced facesheets using higher-order structural theory", Compos. Struct., 127, 340-355.
DOI
|
30 |
Sankar, A., Natarajan, S., Haboussi, M., Ramajeyathilagamc, K. and Ganapathi, M. (2014), "Panel flutter characteristics of sandwich plates with CNT reinforced facesheets using an accurate higher-order theory", J. Fluid. Struct., 50, 376-391.
DOI
|
31 |
Seresta, O. (2007), "Buckling, flutter, and postbuckling optimization of composite structures", PHD Thesis, Aerospace Engineering, Virginia Polytechnic Institute and State University.
|
32 |
Shiau, L.C., Kuo, S.Y. and Liu, Y.P. (2012), "Aerothermoelastic analysis of composite laminated plates", Compos. Struct., 94, 1982-1990.
DOI
|
33 |
Shin, W.H., Oh, I.K. and Lee, I. (2009), "Nonlinear flutter of aerothermally buckled composite shells with damping treatments", J. Sound Vib., 324, 556-569.
DOI
|
34 |
Sohn, K.J. and Kim, J.H. (2009), "Nonlinear thermal flutter of functionally graded panels under a supersonic flow", Compos. Struct., 88, 380-387.
DOI
|
35 |
Song, Z.G. and Li, F.M. (2014), "Aeroelastic analysis and active flutter control of nonlinear lattice sandwich beam", Nonlin. Dyn., 76(1), 57-68.
DOI
|
36 |
Song, Z.G. and Li, F.M. (2016), "Aerothermoelastic analysis of lattice sandwich composite panels in supersonic airflow", Meccanica, 51(4), 877-891.
DOI
|
37 |
Thai, H.T., Nguyen, T.K., Vo, T.P. and Lee, J. (2014), "Analysis of functionally graded sandwich plates using a new first-order shear deformation theory", Eur. J. Mech. A/Solid., 45, 211-225.
DOI
|
38 |
Zhao, M.H. and Zhang, W. (2014), "Nonlinear dynamics of composite laminated cantilever rectangular plate subject to third-order piston aerodynamics", Acta Mech., 225, 1985-2004.
DOI
|
39 |
Wang, Q. (2003), "On complex flutter and buckling analysis of a beam structure subjected to static follower force", Struct. Eng. Mech., 16(5), 533-556.
DOI
|
40 |
Yang, Z., Zhou, J. and Gu, Y. (2014), "Integrated analysis on static dynamic aeroelasticity of curved panels based on a modified local piston theory", J. Sound Vib., 333, 5885-5897.
DOI
|
41 |
Zhong, C. and Reimerdes, H.G. (2007), "Stability behavior of cylindrical and conical sandwich shells with flexible core", J. Sand. Struct. Mater., 9, 143-166.
DOI
|