For supersonic and hypersonic wind tunnels a diffuser efficiency, td, can be defined as the ratio of
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For supersonic and hypersonic wind tunnels a diffuser efficiency, t\d, can be defined as the ratio of the total pressures at the diffuser exit and nozzle reservoir, divided by the total pressure ratio across a normal shock at the test-section Mach number. This is a measure of the efficiency of the diffuser relative to normal shock pressure recovery. Consider a supersonic wind tunnel designed for a test-section Mach number of 3.0 which exhausts directly to the atmosphere. The diffuser efficiency is 1.2. Calculate the minimum reservoir pressure necessary for running the tunnel.
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Mehwish Aziz
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