A supersonic diffuser for air (y%3D1.4) has an arca ratio of 0.416 with an inlet Mach number of 2.4 (design value). Determine the exit Mach number and the design value of the pressure ratio across the diffuser for isentropic flow. At an off-design value of the inlet Mach number (2.7) a normal shock occurs inside the diffuser. Determine the upstream Mach number and area ratio at the section where the shock occurs and pressure ratio across the diffuser.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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A supersonic diffuser for air (y%3D1.4) has an arca ratio of 0.416 with an inlet Mach number
of 2.4 (design value). Determine the exit Mach number and the design value of the
pressure ratio across the diffuser for isentropic flow. At an off-design value of the inlet
Mach number (2.7) a normal shock occurs inside the diffuser. Determine the upstream
Mach number and area ratio at the section where the shock occurs and pressure ratio
across the diffuser.
Transcribed Image Text:A supersonic diffuser for air (y%3D1.4) has an arca ratio of 0.416 with an inlet Mach number of 2.4 (design value). Determine the exit Mach number and the design value of the pressure ratio across the diffuser for isentropic flow. At an off-design value of the inlet Mach number (2.7) a normal shock occurs inside the diffuser. Determine the upstream Mach number and area ratio at the section where the shock occurs and pressure ratio across the diffuser.
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