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(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
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 and total temperature of . 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.


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Given: Exit to entry area ratio (A/A*) = 4.0 Free stream Mach number (M1) = 2.0 Total pressure    To...
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