Jack J M, Adam J C, Andrew R C. Aerothermoelastic modeling considerations for hypersonic vehicles, AIAA-2009-7397[R]. Reston: AIAA, 2009.
[2]
Falkiewicz N J, Cesnik C E S, Crowell A R, et al. Reduced order aerothermoelastic framework for hypersonic vehicle control simulation, AIAA-2010-7928[R]. Reston: AIAA, 2010.
[3]
Vosteen L F, Fuller K E.Behavier of a cantilever plate under rapid heating conditions, NACA RM L55E2[R]. Washington, D. C.: NACA, 1955.
[4]
Richard A, Pride L, Ross L.Some effects of rapid heating on box beam[C]//NACA Conference on Aircraft Loads, Flutter and Structures. Washington, D.C.: NACA, 1955: 489-495.
[5]
Mcintyre K L.Vibration testing during high heat rates, RTD-TDR-63-4197, Part1[R].Hampton: NASA Langley Research Center, 1963.
[6]
Vosteen L F, McWithey R R, Thomson R G. Effect of transient heating on vibration frequencies of some simple wing structures, NACA Technical Note 4054[R]. Washington, D. C.: NACA, 1957.
[7]
Spivey N D. High-temperature modal survey of a hot-structure control surface[C]//The 27th International Congressof the Aeronautical Sciences, 2010.
[8]
Wu D F, Zhao S G, Pan B, et al. Reserch on thermal-vibration joint test for wing structure of high-speed cruise missile[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(9): 1633-1642 (in Chinese). 吴大方, 赵寿根, 潘兵, 等. 高速巡航导弹翼面结构热振联合试验研究[J]. 航空学报, 2012, 33(9): 1633-1642.
[9]
Wu D F, Zhao S G, Pan B, et al. Experiment study on high temperature thermal-vibration characteristics for hollow wing structure of high-speed flight vehicles[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(4): 598-605 (in Chinese). 吴大方, 赵寿根, 潘兵, 等. 高速飞行器中空翼结构高温热振动特性试验研究[J]. 力学学报, 2013, 45(4): 598-605.
[10]
Su H C, Qian Y B, Li Z W, et al. The study of rudder thermo-modal test technique[J]. Structure & Environment Engineering, 2011, 38(5): 18-24 (in Chinese). 苏华昌, 骞永博, 李增文, 等. 舵面热模态试验技术研究[J]. 强度与环境, 2011, 38(5): 18-24.
[11]
Xiao N F, Liu Y Q. Research of control technology in thermal-vibration test[J]. Structure & Environment Engineering, 2012, 39(2): 53-57 (in Chinese). 肖乃风, 刘永清. 热振联合试验控制技术研究[J]. 强度与环境, 2012, 39(2): 53-57.
[12]
Shi Z Y, Law S S. Identification of linear time-varying dynamical systems using Hilbert transform and EMD method[J]. Journal of Application Mechanics, 2007, 74(5): 223-230.
[13]
Xu X Z, Hua H X, Zhang Z Y, et al. Time-varying modal frequency identification by using time-frequency representation[J]. Journal of Vibration and Shock, 2002, 21(2): 36-44 (in Chinese). 续秀忠, 华宏星, 张志谊, 等. 应用时频表示进行结构时变模态频率辨识[J]. 振动与冲击, 2002, 21(2): 36-44.
[14]
Shi Z Y, Shen L. Parameter identification of linear time-varying dynamical system based on wavelet method[J]. Journal of Vibration, Measurement & Diognosis, 2008, 28(2): 108-112 (in Chinese). 史治宇, 沈林. 基于小波方法的时变动力系统参数识别[J]. 振动测试与诊断, 2008, 28(2): 108-112.
[15]
Xu X Z, Zhang Z Y. Decomposition of time-varying modal by time-frequency filter[J]. Noise and Vibration Control, 2005(5): 15-17 (in Chinese). 续秀忠, 张志谊. 基于时频滤波的时变模态分解方法[J]. 噪声与振动控制, 2005(5): 15-17.
[16]
Yu K P. Study on time-varying structural dynamics numerical algorithm and modal parameter identification method[D]. Harbin: Harbin Institute of Technology, 2000 (in Chinese). 于开平. 时变结构动力学数值方法及其模态参数识别方法研究[D]. 哈尔滨: 哈尔滨工业大学, 2000.
[17]
Xu X Z, Zhang Z Y, Hua H X, et al. Identification of time-variant modal parameters by a time-varying parameter approach[J]. Acta Aeronautica et Astronautica Sinica, 2003, 24(3): 230-233 (in Chinese). 续秀忠, 张志谊, 华宏星, 等. 应用时变参数建模方法辨识时变模态参数[J]. 航空学报, 2003, 24(3): 230-233.
[18]
The Editor Committee of "China Aeronautical Material Handbook". China aeronautical material handbook: Vol. 4[M]. 2nd ed. Beijing: China Standards Press, 2001: 74-82 (in Chinese). 《中国航空材料手册》编辑委员会. 中国航空材料手册第4卷,钛合金、铜合金[M]. 2版. 北京: 中国标准出版社, 2001: 74-82.
