[1] Parka JS, Kima JH, Moon SH (2005) Thermal post-buckling and flutter characteristics of composite plates embedded with shape memory alloy fibers. Comp Part B: Eng 36 (8): 627-636.

[2] Fakoor M, Mehri Khansari N (2018) General mixed mode I/II failure criterion for composite materials based on matrix fracture properties. Theo and App Fract Mech 96: 428-442.

[3] Dowell EH (1966) Nonlinear oscillations of a fluttering plate. AAA 4: 1267-1275.

[4] Dowell EH (1967) Nonlinear oscillations of a fluttering plate II. AAA: 1856-1862.

[5] Xue DY, Mei CH (1993) Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow. AIAA 31: 154-162.

[6] Zhou RC, Xue DY, Mei Ch (1994) Finite element time domain—modal formulation for nonlinear flutter of composite panels. AIAA 32 (10): 2044-2052.

[7] Librescu L, Marzocca P, Silva WA (2004) Linear/nonlinear supersonic panel flutter in a high-temperature field. Jou of Aircr 41: 918-924.

[8] Navazi HM, Haddadpour H (2006) Aero-thermoelastic stability of functionally graded plates. Com Stru 80 (4): 580-587.

[9] Song ZG, Li FM (2014) Aerothermoelastic analysis of nonlinear composite laminated panel with aerodynamic heating in hypersonic flow. Comp: Part B 56: 830-839.

[10] موسی زاده ح، قدیری دهکردی ب، راسخ م (1394) بررسی آیروترموالاستیسیته پوسته با خمش استوانه‌ای به روش حجم محدود و باقی‌مانده وزنی گلرکین. مجله مکانیک تربیت مدرس دوره 322-312 :(8)15.

[11] Jiang G, Li F (2018) Aerothermoelastic analysis of composite laminated trapezoidal panels in supersonic airflow. Comp Stru 200: 313-327.

[12] Chen WH, Lin HC (1985) Flutter analysis of thin cracked panels using the finite element method. AIAA 23(5): 795-801.

[13] Pidaparti RMK (1997) Free vibration and flutter of damaged composite panels. Comp Stru 38(1-4): 477-481.

[14] Wang K, Inman DJ, Farrar CR (2005) Crack-induced Changes in Divergence and Flutter of Cantilevered Composite Panels. Stru Hea Moni 4: 377-392.

[15] Natarajan S, Ganapathi M, Bordas S (2013) Supersonic flutter analysis of thin cracked functionally graded material plates. Fron in Aero Eng 2(2): 91-97.

[16] AsadiGorgi H, Dardel M, Pashaei MH (2015) Effect of all-over part-through crack on aeroelastic characteristics of rectangular panels. App Math Mod 39(23-24): 7513-7536.

[17] Abdullah NA, Sosaa J LC, Akbar M (2018) Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method. Comp Stru 202: 151-161.

[18] Rice JR, Levy N (1972) The part through surface crack in an elastic plate. App Mech 39(1): 185-194.

[19] Wu GY, Shih YSH (2005) Dynamic instability of rectangular plate with an edge crack. Compu and Stru 84(1-2): 1-10.

[20] Israr A, Cartmell MP, Manoach E, Trendaf I (2009) Analytical Modeling and Vibration Analysis of Partially Cracked Rectangular Plates With Different Boundary Conditions and Loading. App Mech 76: 11005-11013.

[21] Ismail R, Cartmell MP (2013) An investigation into the vibration analysis of a plate with a surface crack of variable angular orientation. Sou and Vibr 331(12): 2929-2948.

[22] Bose T, Mohanty AR (2013) Vibration analysis of a rectangular thin isotropic plate with a part-through surface crack of arbitrary orientation and position. Soun and Vibr 332(26): 7123-7141.

[23] Diba F, Esmailzadeh E , Younesian D (2014) Nonlinear vibration analysis of isotropic plate with inclined part-through surface crack. Nonlin Dyna 78(4): 2377-2397.

[24] Joshi PV, Jain NK , Ramtekkar GD (2015) Effect of thermal environment on free vibration of cracked rectangular plate: An analytical approach. Th-Wal Stru 91: 38-49.

[25] Joshi PV, Jain NK , Ramtekkar GD, Virdi GS (2016) Vibration and buckling analysis of partially cracked thin orthotropic rectangular plates in thermal environment. Th-Wal Stru 109: 143-158.

[26] Gupta A, Jaina NK, Salhotra R, Rawani AM, Joshi PV (2016) Effect of fibre orientation on non-linear vibration of partially cracked thin rectangular orthotropic micro plate: An analytical approach. Mech Scie 105: 378-397.

[27] Moazzez K, Saeidi Googarchin H, Sharifi SMH (20118) Natural frequency analysis of a cylindrical shell containing a variably oriented surface crack utilizing Line-Spring model. Th-Wa Stru 125: 63-75.

[28] Reddy JN (2004) Mechanics of laminated composite plates and shells, theory and analysis, Second ed, CRC Press, Florida.

[29] Leissa W (1969) Vibration of Plates. NASA 70N18461, Washington DC, United States.

[30] Joshi PV, Jain NK, Ramtekkar GD (2014) Analytical modeling and vibration analysis of internally cracked rectangular plates. Sou and Vibr 333(22): 5851-5864.

[31] Kouchakzadeha MA, Rasekh M, Haddadpour H (2010) Panel flutter analysis of general laminated composite plates. Comp Struc 92(12): 2906-2915.