[1] Jordan PF (1956) The physical nature of panel flutter. Aero Digest 3:34-38.
[2] Song ZG, Li FM (2008), Active aeroelastic flutter analysis and vibration control of supersonic beams using the piezoelectric actuator/sensor pairs. Smart Mater Struc 20(55013).
[3] Samadpour M, Asadi H, Wang Q (2016) Nonlinear aero-thermal flutter postponement of supersonic laminated composite beams with shape memory alloys. Eur J Mech A-Solid 57(0): 18-28.
[4] Tsushima N, Su W (2017) Flutter suppression for highly flexible wings using passive and active piezoelectric effects. Aerosp Sci Technol 65(0): 78-89.
[5] Bahaadini R, Saidi A (2019) Aerothermoelastic flutter analysis of pre-twisted thin-walled rotating blades reinforced with functionally graded carbon nanotubes. Eur J Mech A-Solid 75(0): 285-306.
[6] Abdullatif M, Mukherjee R (2019) Divergence and flutter instabilities of a cantilever beam subjected to a terminal dynamic moment. J Sound Vib 1(1): 1-18.
[7] Chai YY, Song ZG, Li FM (2017) Active aerothermoelastic flutter suppression of composite laminated panels with time-dependent boundaries. Compos Struct 179: 61-76.
[8] Gee DJ, Sipcic SR (1999) Coupled thermal model for non-linear panel flutter. AIAA J 37(5): 624-649.
[9] Li H, Motamedi P, Hogan J (2019) Characterization and mechanical testing on novel (γ + α2) – TiAl/Ti3Al/Al2O3 cermet. Mat Sci Eng A-Struct 750: 152-163.
[10] Wang X, Gao J, Hua H, Zhang H, Liang L, Javaid K, Wang L (2017) High-temperature tolerance in WTi-Al2O3 cermet-based solar selective absorbing coatings with low thermal emissivity. Nano Energy 37: 232-241.
[11] Li F, Song Z, Sun C (2015) Aeroelastic properties of sandwich beam with pyramidal lattice core considering geometric nonlinearity in the supersonic airflow. Acta Mech Solida Sin 28(6): 639-646.
[12] Zhang ZJ., Han B, Zhang QC, Jin F (2017) Free vibration analysis of sandwich beams with honeycomb-corrugation hybrid cores. Compos Struct 171: 335-344.
[13] Song ZG, Li FM (2016) Flutter and buckling characteristics and active control of sandwich panels with triangular lattice core in supersonic airflow. Compos Part B-Eng 108: 334-344.
[14] Eloy F, Gomes G, Ancelotti JR A, Cunha JR, Bombard A, Junqueira D (2018) Experimental dynamic analysis of composite sandwich beams with magnetorheological honeycomb core. Eng Struct 176: 231-242.
[15] Boucher MA, Smith CW, Scarpa F, Rajasekaran R, Evans KE (2013) Effective topologies for vibration damping inserts in honeycomb structures. Compos Struct 106: 1-14.
[16] Sakar G, Bolat FC (2015) The free vibration analysis of honeycomb sandwich beam using 3D and continuum model. Int J Mech Mechatronics Eng 9(6): 1077-1081.
[17] Mukhopadhyay T, Adhikari SS (2016) Free-vibration analysis of sandwich panels with randomly irregular honeycomb core. J Eng Mech 06016008: 1-5.
[18] McAdam GD (1967) The mechanical properties of cermets with a metallic matrix. Powder Metall 10(20).
[19] Ruzzene M, Scarpa F (2003) Control of wave propagation in sandwich beams with auxetic core.J Intel Mater Sys Struct14:443-453.
[20] Mead DJ, Markus SS (1969) The forced vibration of a three-layer, damped sandwich beam with arbitrary boundary conditions. J Sound Vib 10(2): 163-175.
[21] Rao SS (2007) Vibration of continuous systems. 5th edn. John Wiley & Sons, Inc, New Jersey.
[22] Hasheminejad SM, Nezami M, Aryaee Panah ME (2012) Supersonic flutter suppression of electrorheological fluid-based adaptive panelsresting on elastic foundations using sliding mode control. Smart Mater Struct21(045005).
[23] Dorsey JT (2002) Metallic thermal protection system technology development: Concepts, requirements and assessment overview. 40th Aerospace Science Meeting, AIAA2002-0502.
[24] Esen I (2011) Dynamic response of a beam due to an accelerating moving mass using moving finite element approximation. Math Comput Appl 16(1): 171-182.
)