摘要
The precondition of solving life prediction and life extension for airplane structures is to work out a typical load-time history, i.e. load-spectrum, which can simulate airplane's real service situation. This is the basis of theory analysis and whole-size structure fatigue test. In view of this, the data treatment and the compilation procedure of median stochastic load-spectrum are discussed. The data treatment expert system for median stochastic load-spectrum is created on this basis. It includes system framework design, data description and parameter configuration, implementation process and database design, etc. The research achievement has been used for load-spectrum data treatment and compilation for airplane, aeroengine, airplane landing gear and main fighting tank, etc.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 428-431 |
| 页数 | 4 |
| 期刊 | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| 卷 | 26 |
| 期 | 4 |
| 出版状态 | 已出版 - 8月 2000 |
| 已对外发布 | 是 |
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