(Solved): Consider an isentropic flow through a subsonic diffuser with an exit to entry area ratio of 4.0. Th ...
Consider an isentropic flow through a subsonic diffuser with an exit to entry area ratio of 4.0. The free stream Mach number is equal to 2.0 with total pressure of 1.0atm and total temperature of 300K. If there is a standing normal shock before the entry of the diffuser, calculate the Mach number and temperature at the exit of the diffuser.