MARC状态：已编 文献类型：西文图书 浏览次数：38
- 题名/责任者:
- New analytical methods for the prediction of fatigue crack growth under realistic loading / by H.H. van der Linden, A.U. de Koning and C.J. Lof.
- 出版发行项:
- [Amsterdam : 1983.
- 载体形态项:
- 23 p. : ill. ; 26 cm.
- 丛编说明:
- NLR MP ; 82055 U
- 丛编统一题名:
- Nationaal Lucht- en Ruimtevaartlaboratorium ; MP 82055 U.
- 个人责任者:
- Linden, H.H. van der.
- 附加个人名称:
- Koning, A.U. de.
- 附加个人名称:
- Lof, C.J.
- 论题主题:
- Airframes-Fatigue.
- 中图法分类号:
- V215
- 一般附注:
- This report has been prepared for publication in special issue of the International Journal of Vehicle Design.
- 一般附注:
- This issue is entitled "Application of new techniques for analysis and design of aircraft structures."
- 一般附注:
- The investigations mentioned in this paper have been carried out under contract with the Netherlands Agency for Aerospace Programs (NIVR)
- 一般附注:
- Contract numbers 1777, 1822, 1823 and 1776.
- 书目附注:
- Includes bibliographical references.
- 摘要附注:
- After a discussion of some aspects of aircraft design philosophy and the fatigue phenomenon, two analytical techniques for prediction of crack growth rates are described. The first method includes a model for prediction of fatigue crack growth in aluminium alloy sheet specimens subjected to service loading conditions. The second method involves the application of linear elastic fracture mechanics to three dimensional crack growth prediction under constant amplitude loading. Predictions are compared with experimental results.
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