共 70 条
[1]
Asundi A(1997)Fiber metal laminates: an advanced material for future aircraft J Mater Process Technol 63 384-394
[2]
Choi AYN(2011)A review: fibre metal laminates, background, bonding types and applied test methods Mater Des 32 3671-3685
[3]
Avcu E(1999)Towards application of fibre metal laminates in large aircraft Aircr Eng Aerosp Technol 71 558-570
[4]
Vlot A(2016)Research progress of ultra-light fiber metal laminates Aeronaut Manuf Technol 23 133-136
[5]
Vogelesang LB(2013)Application and property analysis of fiber-metal laminate for aircraft manufacturing Aeronaut Manuf Technol 1 133-139
[6]
DeVries TJ(1959)Damping of flexural waves by a constrained viscoelastic layer Acoust Soc Am J 31 952-962
[7]
Wu G(1993)A vibration and damping analysis of circular plates with constrained damping layer treatment Comput Struct 49 269-274
[8]
Pan Y(2004)Constrained damping layer treatments: finite element modeling J Vib Control 10 575-595
[9]
Zhang Z(2011)Theory of vibratory bending for elastic and viscoelastic layered finite-length beams J Appl Mech 32 881-886
[10]
Huang Z(2012)Dynamic analysis and design of laminated composite beams with multiple damping layers AIAA J 31 736-745