Numerical investigation of the loading frequency for fatigue test of C/SiC materials

被引:0
|
作者
Zhou Y.-D. [1 ,2 ]
Fei Q.-G. [1 ,3 ]
Wu S.-Q. [3 ]
Tan Z.-Y. [4 ]
机构
[1] Department of Engineering Mechanics, Southeast University, Nanjing
[2] Department of Mechanical Engineering, Northwestern University, Evanston, 60208, IL
[3] Jiangsu Key Laboratory of Engineering Mechanics, Nanjing
[4] State Key Laboratory of Space Physics, Beijing
关键词
Acoustic fatigue; C/SiC materials; Frequency-dependence; Loading frequency; S-N curve;
D O I
10.16385/j.cnki.issn.1004-4523.2016.06.006
中图分类号
学科分类号
摘要
The S-N curve of material and dynamic stress responses are two necessary elements for acoustic fatigue life assessment of hot structures. However, the S-N curves of C/SiC material for hot structures are of great frequency-dependence. In order to obtain the proper S-N curve of C/SiC material for the fatigue life assessment of typical hot structures subjected to the random acoustic loading, the level-crossing problem of a random signal was analyzed. The expected level-up crossing was deduced. The zero-up crossing was demonstrated to characterize the expected frequency of a random process. And the zero-up crossing can be calculated using the power spectral density function of the process. The finite element model of a stiffened panel was constructed and the power spectral density of stress responses of the panel at three representative locations were calculated under the excitation of acoustic loading. Numerical analysis was conducted to examine the accuracy of zero-up crossing to represent the average cycles per second of a Gaussian-distributed random signal. Numerical results show a good agreement. The maximum of the three zero-up crossings is 532 Hz. Thus, the fatigue test to obtain S-N data need to be conducted at the loading frequency of 532 Hz as far as possible. © 2016, Nanjing Univ. of Aeronautics an Astronautics. All right reserved.
引用
收藏
页码:985 / 991
页数:6
相关论文
共 23 条
  • [1] Pichon T., Barreteau R., Soyris P., Et al., CMC thermal protection system for future reusable launch vehicles: Generic shingle technological maturation and tests, Acta Astronautica, 65, 1, pp. 165-176, (2009)
  • [2] Lu Q., Hu L., Luo X., Et al., Development of ceramic composite and hot structures for hypersonic vehicles, Journal of the Chinese Ceramic Society, 41, 2, pp. 251-260, (2013)
  • [3] Zhang K., Xue P., Hu H., Et al., Vibration-fatigue life analysis of thin panels under loads containing high frequency components, Mechanical Science and Technology for Aerospace Engineering, 31, 4, pp. 639-642, (2012)
  • [4] Deng W., Yu W., Shi X., Comparative research between random vibration test and acoustic test for small-satellite, Spacecraft Engineering, 18, 1, pp. 79-82, (2009)
  • [5] Cunningham P.R., White R.G., A review of analytical methods for aircraft structures subjected to high-intensity random acoustic loads, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 218, 3, pp. 231-242, (2004)
  • [6] Quiroz R., Embler J., Jacobs R., Et al., Air Vehicle Integration and Technology Research (AVIATR), Task Order 0023: Predictive Capability for Hypersonic Structural Response and Life Prediction: Phase 2-Detailed Design of Hypersonic Cruise Vehicle Hot-Structure, (2012)
  • [7] Vassilopoulos A.P., Fatigue Life Prediction of Composites and Composite Structures, (2010)
  • [8] Kharrazi M.R., Sarkani S., Frequency-dependent fatigue damage accumulation in fiber-reinforced plastics, Journal of Composite Materials, 35, 21, pp. 1924-1953, (2001)
  • [9] Ruggles-Wrenn M.B., Hetrick G., Baek S.S., Effects of frequency and environment on fatigue behavior of an oxide-oxide ceramic composite at 1200℃, International Journal of Fatigue, 30, 3, pp. 502-516, (2008)
  • [10] Ruggles-Wrenn M.B., Christensen D.T., Chamberlain A.L., Et al., Effect of frequency and environment on fatigue behavior of a CVI SiC/SiC ceramic matrix composite at 1200℃, Composites Science and Technology, 71, 2, pp. 190-196, (2011)