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...
保存先:
| 第一著者: | |
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| 共著者: | , |
| フォーマット: | 図書 |
| 言語: | English |
| 出版事項: |
Melbourne :
DSTO Aeronautical and Maritime Research Laboratory,
1996.
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| シリーズ: | Technical report (Defence Science and Technology Organisation (Australia)) ;
DSTO-TR-0330. |
| 主題: | |
| オンライン･アクセス: | http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0330.pdf |
インターネット
http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0330.pdfCARM 1 Store
| 請求記号: |
A2:AH26H0 F01289 |
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| 所蔵 1 | 利用可 予約する |