文献
J-GLOBAL ID:201502203233004828
整理番号:15A0392283
軸方向引張試験下の航空機で用いられる2024-T3Al合金板の残留極限強さに及ぼす局所くぼみの影響
The effect of local dents on the residual ultimate strength of 2024-T3 aluminum alloy plate used in aircraft under axial tension tests
著者 (9件):
LI Zhigang
(Beijing Jiaotong Univ., Beijing, CHN)
,
LI Zhigang
(Beijing Aeronautical Sci. & Technol. Res. Inst. of Commercial Aircraft Corp. of China, Ltd., Beijing, CHN)
,
ZHANG Dingni
(Shanghai Normal Univ., Shanghai, CHN)
,
PENG Chunlei
(China North Vehicle Res. Inst., Beijing, CHN)
,
MA Chunsheng
(Tsinghua Univ., Beijing, CHN)
,
ZHANG Jinhuan
(Tsinghua Univ., Beijing, CHN)
,
HU Zhongmin
(Beijing Aeronautical Sci. & Technol. Res. Inst. of Commercial Aircraft Corp. of China, Ltd., Beijing, CHN)
,
ZHANG Jiazhen
(Beijing Aeronautical Sci. & Technol. Res. Inst. of Commercial Aircraft Corp. of China, Ltd., Beijing, CHN)
,
ZHAO Yanan
(Beijing Inst. of Technol., Beijing, CHN)
資料名:
Engineering Failure Analysis
(Engineering Failure Analysis)
巻:
48
ページ:
21-29
発行年:
2015年02月
JST資料番号:
W0684A
ISSN:
1350-6307
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
イギリス (GBR)
言語:
英語 (EN)