Wu Zhen, Chen Wanji. A C0-type higher-order theory for bending analysis of laminated composite and sandwich plates[J]. Composite Structures, 2010,92:653-661.
[2]
Myers D E, Martin C J, Blosser M L. Parametric weight comparison of advanced metallic, cream tile, and ceramic blanket thermal protection systems, NASA/TM-2000-210289[R]. Hampton, USA: Langley Research Center, 2000.
[3]
William L K. Heat shielding characteristics and thermostructural performance of a superalloy honeycomb sandwich thermal protection system (TPS), NASA/TP-2004-212024[R]. Washington D.C.: NASA, 2004.
[4]
刘振祺,梁伟,杨嘉陵,等.MTPS蜂窝夹芯结构传热性能及热应力分析[J].航空学报,2009,30(1):86-91. Liu Zhenqi, Liang Wei, Yang Jialing, et al. Analysis of thermal and mechanical properties of honeycomb structure of MTPS[J]. Acta Aeronautica ET Astronautica Sinica, 2009,30(1):86-91.(in Chinese)
[5]
刘宝军.金属蜂窝夹芯板力热耦合作用下的数值模拟[D].哈尔滨:哈尔滨工程大学,2011. Liu Baojun. The simulation of metal honeycomb sandwich panel under thermomechanical coupling[D]. Harbin: Herbin Engineering University, 2011.(in Chinese)
[6]
KamranD, Max B L, Kathryn W E. Displacements of metallic thermal protection system panels during reentry, AIAA-2006-2948[R]. Hampton, USA: Langley Research Center, 2006.
[7]
Romanoff J, Varsta P. Bending response of web-core sandwich plates[J]. Composite Structures, 2007,81:292-302.