Effect of plate thickness on the in-plane and through-thickness stresses at a hole /
Holes exist in metallic aircraft structures for either design or construction reasons and their stress concentrating effect is such that they are common regions of fatigue crack initiation. A combined experimental and numerical study has been carried out to examine the influence of thickness on the...
محفوظ في:
| المؤلف الرئيسي: | |
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| مؤلفون مشاركون: | , |
| التنسيق: | كتاب |
| اللغة: | English |
| منشور في: |
Melbourne :
DSTO Aeronautical and Maritime Research Laboratory,
1996.
|
| سلاسل: | Technical report (Defence Science and Technology Organisation (Australia)) ;
DSTO-TR-0330. |
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0330.pdf |
الانترنت
http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0330.pdfCARM 1 Store
| رقم الطلب: |
A2:AH26H0 F01289 |
|---|---|
| النسخة 1 | متاح أحجز النسخة |