日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
特集 先進航空宇宙材料の現状と問題点
繰返しモードII荷重下における疲労き裂の伝播挙動
藤本 浩司永野 正人茅野 雅久
著者情報
ジャーナル フリー

2000 年 48 巻 556 号 p. 320-325

詳細
抄録

The behaviour of the fatigue crack propagation under the repeated mode II loading was investigated using the rolled plate specimens with a fatigue precrack. Tests on the alminium alloys (7075-T 6, 2017-T 4) and the mild steel (SS 400) were conducted, and the macroscopic crack paths and the microscopic fracture surfaces were examined. In these tests under the repeated mode II loading to the precrack, two modes of the fatigue crack growth were observed ; the mode I crack growth and the mode II crack growth. In 2017-T 4 specimens, the mode II crack growth was always observed while in SS 400, only the mode I crack growth was observed. However, in 7075-T 6 specimens, the mode I growth was observed in low ΔKII and the mode II growth in high ΔKII.

著者関連情報
© 2000 一般社団法人 日本航空宇宙学会
前の記事 次の記事
feedback
Top