Compressible Flow Components Ideal vs Real Operation Analysis

The subsonic nozzle, diffuser and thrust analysis is presented only for the air as the working fluid.  The technical performance of mentioned compressible flow components is presented with a given relationship between temperature and pressure as a function ofthe  Mach Number and isentropic nozzle and diffuser efficiency.

This course material provides the compressible flow components T - s diagrams and their major performance trends (stagnation over static temperature and pressure ratio values) are plotted in a few figures as a function of the Mach Number.

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