Investigation on vibration fatigue crack growth behavior of notched cantilever beams
Aviation aircraft will be subjected to a large number of complex random vibration loads during service， and its structure is prone to vibration fatigue，which leads to damage or even failure，which can cause serious losses. The stress intensity factor（SIF）solution method for cracked beams under random...
| الحاوية / القاعدة: | Hangkong gongcheng jinzhan |
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| المؤلفون الرئيسيون: | , , , , |
| التنسيق: | مقال |
| اللغة: | الصينية |
| منشور في: |
Editorial Department of Advances in Aeronautical Science and Engineering
2024-10-01
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| الموضوعات: | |
| الوصول للمادة أونلاين: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2024199 |