On shock layer method for the hypersonic flow problems

Chernyi's series method^1] is not proper for the case that(–1)/(+1)2/(+1)×M ²sin² (=c_p/c_v — adiabatic index number, M — Mach number, — shock incidence). In this paper, we only suppose that in the neighbour of the shock, there exists a shock layer in which the density of the gas is very big, but we do not remove the case that (–1)/(+1)2/(+1)M ²sin².