• On diffuser efficiency in compressible flow

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      https://www.ias.ac.in/article/fulltext/seca/022/02/0067-0074

    • 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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