High Speed Flight and Partial Differential Equations

作     者：Shuxing CHEN Shuxing CHEN

作者机构：School of Mathematical SciencesFudan UniversityShanghai200433China 

出 版 物：《Chinese Annals of Mathematics,Series B》 (数学年刊（B辑英文版）)

年 卷 期：2022年第43卷第5期

页      面：855-868页

核心收录：

学科分类：07[理学] 080103[工学-流体力学] 08[工学] 080104[工学-工程力学] 070104[理学-应用数学] 0701[理学-数学] 0801[工学-力学（可授工学、理学学位）] 

主　　题：Supersonic flow Euler system Potential flow Conservation laws Shock 

摘      要：Aircraft comes out at the beginning of the last century. Accompanied by the progress of high speed flight the theory of partial differential equations has been greatly developed. This paper gives a brief review on the history of applications of partial differential equations to the study of supersonic flows arising in high speed flight.