• On diffuser efficiency in compressible flow

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    • Keywords


      Mach Number; Compressible Flow; Stagnation Pressure; Pressure Recovery; Exit Section

    • Abstract


      An expression for diffuser efficiency in compressible flow has been developed. Experimental procedures for the determination of the efficiency are outlined and the steps for calculating it from the experimental data are indicated.

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© 2021-2022 Indian Academy of Sciences, Bengaluru.