摘要
In this paper, we prove the local existence, uniqueness and stability of a supersonic shock for the supersonic isothermal incoming flow past a curved cone. Major difficulties include constructing an appropriate solution and treatincg the Neumann boundary conditions and local stability condition.
In this paper, we prove the local existence, uniqueness and stability of a supersonic shock for the supersonic isothermal incoming flow past a curved cone. Major difficulties include constructing an appropriate solution and treatincg the Neumann boundary conditions and local stability condition.
基金
supported by Scientific Research Fund of Nanjing Institute of Technology (Grant No.YKJ201339)
National Natural Science Foundation of China (Grant Nos.11371189 and 11101190)
the Priority Academic Program Development of Jiangsu Higher Education Institutions
