| 飞机损伤容限和耐久性设计技术的发展 |
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| 引用本文： | 李克唐. 飞机损伤容限和耐久性设计技术的发展[J]. 航空学报, 1986, 7(6): 531-538 |
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| 作者姓名： | 李克唐 |
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| 作者单位： | 成都飞机公司发展部 |
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| 摘 要： | 本文评介并讨论了以下问题:两类经验教训;设计思想的发展--五种模式;损伤容限和耐久性设计技术的特征;飞机设计应用实例;需要进一步研究的若干问题。
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| 关 键 词： | |
| 收稿时间： | 1986-02-20; |
DEVELOPMENT OF DAMAGE TOLERANCE AND DURABILITY DESIGN TECHNOLOGY |
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| Li Ketang. DEVELOPMENT OF DAMAGE TOLERANCE AND DURABILITY DESIGN TECHNOLOGY[J]. Acta Aeronautica et Astronautica Sinica, 1986, 7(6): 531-538 |
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| Authors: | Li Ketang |
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| Affiliation: | Development Department, Chengdu Aircraft Company |
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| Abstract: | In this paper, The following problems are reviewed and discussed: Two kinds of experiences and lessons; Development of design conceptionr Characteristics of damage tolerance and durability design technology; practical examples in aircraft design; Some problems to be further studied. |
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