-1)下的動(dòng)態(tài)拉伸試驗(yàn);根據(jù)試驗(yàn)數(shù)據(jù)對(duì)J-C本構(gòu)模型中的應(yīng)變率強(qiáng)化項(xiàng)和熱軟化項(xiàng)進(jìn)行了修正,并標(biāo)定相關(guān)模型參數(shù)。進(jìn)一步開(kāi)展數(shù)據(jù)仿真分析,并對(duì)比試驗(yàn)與仿真的斷裂位置和真應(yīng)力-應(yīng)變曲線,驗(yàn)證失效模型參數(shù)的可靠性。使用SEM對(duì)鎂合金斷口微觀形貌進(jìn)行觀察,探究溫度、應(yīng)變率對(duì)鎂合金失效影響的微觀行為特征,鎂合金在準(zhǔn)靜態(tài)拉伸與動(dòng)態(tài)拉伸過(guò)程中斷口形貌中均發(fā)現(xiàn)了韌窩與解理臺(tái)階,為混合斷裂機(jī)制,且高應(yīng)變速率下解理臺(tái)階稍多,這與鎂合金高應(yīng)變速率下的應(yīng)變敏感性有關(guān);而在高溫拉伸過(guò)程中表現(xiàn)為韌性斷裂。"/>
1.中北大學(xué) 智能武器研究院,山西 太原 030051;2.中北大學(xué) 機(jī)電工程學(xué)院,山西 太原 030051;3.中北大學(xué) 材料科學(xué)與工程學(xué)院,山西 太原 030051;4.火箭軍工程大學(xué) 導(dǎo)彈工程學(xué)院,陜西 西安 710051
TG146.22
國(guó)家自然科學(xué)基金(52205428);中國(guó)博士后科學(xué)基金(2024M754274);山西省應(yīng)用基礎(chǔ)研究計(jì)劃(202303021212180,20210302124206);山西省科技創(chuàng)新領(lǐng)軍人才團(tuán)隊(duì)專項(xiàng)(202204051002001)
1.Intelligent Weapons Research Institute, North University of China, Taiyuan 030051, China;2.School of Mechanical and Electrical Engineering, North University of China, Taiyuan 030051, China;3.School of Materials Science and Engineering, North University of China, Taiyuan 030051, China;4.College of Missile Engineering, Rocket Force University of Engineering, Xi'an 710051, China
The National Natural Science Foundation of China (General Program, Key Program, Major Research Plan),China Postdoctoral Science Foundation,Shanxi Province Applied Basic Research Plan,Special Project for the Leading Talent Teams in Scientific and Technological Innovation in Shanxi Province
郅慧棟,郭保全,丁寧,閆釗鳴,朱家萱,萬(wàn)晨.
DOI:10.12442/j. issn.1002-185X.20240505