针对航空航天薄壁结构在热声载荷作用下的非线性振动响应问题,基于声振耦合理论,采用耦合的有限元/边界元法对四边固支高温合金矩形薄壁结构进行了动力学响应计算。重点研究了薄壁结构在行波加载与扩散场加载条件下的振动应力/应变响应规律,讨论了温升对结构振动响应的影响规律,分析了薄壁结构热屈曲(Thermal-buckling)和跳变(Snap-through)响应特性。通过将薄壁结构在不同温度条件下的振动模态以及动态应变响应的仿真结果与热环境下的声激振试验结果进行对比,表明计算的基频量值及随温度的变化关系与试验结果获得较好的一致性,计算的应变响应与试验测试结果量值相当,验证了热声响应计算方法与模型的有效性。本文研究提出的金属薄壁结构在热声载荷作用下的非线性振动响应计算方法及分析结论对进一步开展热声疲劳寿命预测及动强度设计提供依据。
Abstract
For nonlinear vibration response problems of aerospace thin-walled structures under thermal-acoustic excitations, based on the theory of structural-acoustic coupling, the coupled FEM/BEM method was used to calculate dynamic responses of super-alloy thin-wall rectangular plates with four edges clamped. Researches were mainly focused on the influence of progressive wave and diffused acoustic field on the vibration stress/strain responses of thin-walled structures, the effects of temperature rising on vibration responses of structures were discussed, and the characteristics of thermal-buckling and snap-through of thin-walled structures were analyzed. By comparing simulation results of vibration modals and dynamic strain responses of thin-walled structures in different temperatures with experimental results of thermal-acoustic excitations, it shows that fundamental frequencies and changing trend with the increase of temperature of structures keep a preferable consistency with test results, and strain responses of calculation and experimental results have a good alignment, validating the effectiveness of calculation method and model to thermal-acoustic responses. The calculation method of thin-walled structures nonlinear vibration responses and analysis conclusions presented in this paper will provide references to further carry out thermal-acoustic fatigue life prediction and the dynamic strength design of thin-walled structures.
关键词
金属薄壁结构 /
热声载荷 /
非线性振动响应 /
试验验证
{{custom_keyword}} /
Key words
Metallic thin-walled structures ;Thermal-acoustic loads /
Nonlinear vibration responses /
Experimental verification
{{custom_keyword}} /
{{custom_sec.title}}
{{custom_sec.title}}
{{custom_sec.content}}
参考文献
[1] Lee J. Large-Amplitude Plate Vibration in an Elevated Thermal Environment [R]. Flight Dynamics Directorate, Wright Laboratory Wright-Patterson,1992.
[2] Lee J. Displacement and Strain Histograms of Thermally Buckled Composite Plates in Random Vibration [C]. Structural Dynamics, and Materials Conference and Exhibit, 1996.
[3] Lee J. Displacement and Strain Statistics of Thermally Buckled Plates [C]. Structural Dynamics, and Materials Conference and Exhibit,1999.
[4] Vaicaitis R. Nonlinear response and sonic fatigue of National Aerospace Space Plane surface panels[J]. Journal of Aircraft, 1994, 31 (1): 10-18.
[5] Vaicaitis R. and Kavallieratos PA. Nonlinear response of composite panels to random excitation[C]. Structural Dynamics and Materials Conference,1993.
[6] Lee J. Displacement and strain statistics of thermally buckled plates [C]. Structural Dynamics, and Materials Conference and Exhibit,1999.
[7] Lee J. Displacement and strain histograms of thermally buckled composite plates in random vibration [C]. Structural Dynamics, and Materials Conference and Exhibit, 1996.
[8] Lee Jon. Large-amplitude plate vibration in an elevated thermal environment [R]. Applied Mechanics Reviews, 1992.
[9] Mei C, Dhainaut J M, Duan B, Spottswood S M, et al. Nonlinear random response of composite panels in an elevated thermal environment [R]. 2000
[10] Dhainaut J M, Guo X, Mei C, Spottswood S M and Wolfe H F. Nonlinear random response of panels in an elevated thermal-acoustic environment[J]. Journal of Aircraft, 2003, 40(4): 683-691
[11] Ng C F, Clevenson S A. High-Intensity Acoustic Tests of a Thermally Stressed Plate [J]. Journal of Aircraft, 1991, 28(4): 275-281.
[12] Rizzi S A. Experimental research activities in dynamic response and sonic fatigue of hypersonic vehicle structures at NASA Langley Research Center [C]. Aerospace Sciences Meeting and Exhibit, 1993.
[13] Ng Chung Fai. Design guide for predicting nonlinear random response(including snap-through) of buckled plates [M]. General Books LLC,2011.
[14] Ng Chung Fai and Wentz K R. The prediction and measurement of thermo-acoustic response of plate structures [C]. Structural Dynamics, and Materials Conference,1990.
[15] Ng Chung Fai. Nonlinear and snap-through responses of curved panels to intense acoustic excitation [J]. Journal of Aircraft, 1989, 26(3):281-288.
[16] Jacobson M J. Sonic Fatigue of Advanced Composite Panels in Thermal Environments[J]. Journal of Aircraft 1983, 20(3): 282-288.
[17] Jacobs J H, Gruensfelder C, Hedgecock C E. Thermal Acoustic Fatigue of Ceramic Matrix Composite Materials [C]. Structural Dynamics, and Materials Conference,1993.
[18] Y. D. Sha, Z. J. Gao, F. Xue and J. Y. Li. Influence of Thermal Loading on the Dynamic Response of Thin-Walled Structure under Thermo-Acoustic Loading [J]. Applied Mechanics and Materials, 2011,2-3: 876-881.
[19] Y. D. Sha, Z. Zhang, F. T. Zhao and J. Wei. Estimation of Random Sonic Fatigue Life Based on Peak Probability Density of Von Mises Stress[J]. Advanced Materials Research, 2011,199-200: 913-921.
[20] Sha Y.D., Li J.Y. and Gao Z.J. Dynamic Response of Pre/Post Buckled Thin-Walled Structure under Thermo-Acoustic Loading[J]. Applied Mechanics and Materials, 2011, 80-81: 536-541.
[21] Sha Y.D., Gao Z.J., Xu F. and Li J.Y. Influence of Thermal Loading on the Dynamic Response of Thin-Walled Structure under Thermo-Acoustic Loading[C]. International Conference on Applied Mechanics, Material and Manufacturing, 2011.
[22] Sha Y.D., Xu F. and Gao Z.J. Nonlinear Response of Carbon-Carbon Composite Panels Subjected to Thermal-Acoustic Loadings[J]. Applied Mechanics and Materials, 2012, 117-119:876-881.
[23] Sha Y.D., WeiJ. and Gao Z.J. Nonlinear Characteristics of Thin-walled Structures under Thermo-acoustic Loadings [J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(6): 1336-1346.
沙云东,魏静,高志军.热声载荷作用下薄壁结构的非线性响应特性[J]. 航空学报, 2013, 34(6):1336-1346.
[24] Pates, Carl Stansbbury. Analysis of Random Structure-acoustic Interaction Problems Using Coupled Boundary Element and Finite Element Methods:[D] Old Dominion University, 1994.
[25] M. P. Norton著, 盛元生译. 工程噪声和振动分析基础[M]. 航空工业出版社,1993.
{{custom_fnGroup.title_cn}}
脚注
{{custom_fn.content}}