Research on missile jet-airplane interaction by an experimental method

摘要：

　　Based on the local dynamic similarity theory, the experimental apparatus of modeling missile jet-airplane interaction have been set up.The pressure and temperature test systems have been improved.In order to achieve high accuracy of test results, the heating influence of pressure and temperature has been diminished.Several new structures for controlling the strength of shock wave that acts on airplane body and is caused by missile jet have been designed and tested.The flow mechanism of missile jet-airplane interaction has been well understood and some technical measurements for controlling shock wave have been explored.

关键词： Missile jet-airplane Interaction experimental method Research

作者: Fei-peng ZENG Zhou WEN

作者单位: Army Artillery and Air Defense Force Academy, Nanjing, China

会议类型: 国际会议

会议名称: 2018 International Conference on Defence Technology (2018国际防务技术会议)

会议地点: 北京

会议语种:英文

页码: 670-672

在线出版日期: 2018-10-21（万方平台首次上网日期，不代表论文的发表时间）