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作 者:周峰[1] 刘畅 赵克良[1] 周光明[2] 蔡登安[2] 李康桥[2] 林显巧 ZHOU Feng;LIU Chang;ZHAO Keliang;ZHOU Guangming;CAI Dengan;LI Kangqiao;LIN Xianqiao(Shanghai Aircraft Design and Research Institute,Shanghai,201210,China;State Key Laboratory of Mechanics and Control of Mechanical Structures,Nanjing University of Aeronautics&Astronautics,Nanjing,210016,China)
机构地区:[1]上海飞机设计研究院,上海201210 [2]南京航空航天大学机械结构力学及控制国家重点实验室,南京210016
出 处:《南京航空航天大学学报》2020年第4期639-643,共5页Journal of Nanjing University of Aeronautics & Astronautics
摘 要:提出一种测试结冰界面切向冻粘强度的新方法。设计了新型的拼接式结冰装置,进行圆柱形结冰杆表面的结冰,再通过压缩试验完成切向冻粘强度测试。在上述工作基础上进一步地研究了多个试验因素对切向冻粘强度的影响。试验结果表明:随着接触面积或者冻结时间的增加,切向冻粘强度均呈现先增大后稳定的趋势;随着加载速率的增大,切向冻粘强度值呈现先增加后减小的趋势;在-5^-30℃之间,切向冻粘强度与冻结温度近似为线性关系。A novel method to measure the shear freezing adhesion strength at the ice interface was presented in this paper.A new splicing-type freezing device was designed to complete the freezing process on the surface of the cylindrical ice pole,and the compression experiment was carried out to test the shear freezing adhesion strength.The influence of several experimental factors was further studied on the basis of the above work.Test results show that the shear freezing adhesion strength firstly increases and then stabilizes with the increase of the contact area and the freezing time while the strength firstly increases and then decreases with the increase of the loading rate.The shear freezing adhesion strength changes approximately linearly with the freezing temperature between-5℃and-30℃.
分 类 号:V216.1[航空宇航科学与技术—航空宇航推进理论与工程]
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