The service life of aircraft structural components undergoing random stress cycling was analyzed by the application of fracture mechanics. The initial crack sizes at the critical stress points for the fatigue crack growth analysis were established through proof load tests. The fatigue crack growth r
β¦ LIBER β¦
The contribution of life cycle theory to pastoral premarital and marriage counseling
β Scribed by Mark W. Muncy
- Publisher
- Springer
- Year
- 1983
- Tongue
- English
- Weight
- 593 KB
- Volume
- 31
- Category
- Article
- ISSN
- 0031-2789
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