Advanced Compressible Flow Components Analysis

The ideal subsonic nozzle, diffuser and thrust analysis is presented when air, argon, helium and nitrogen are considered 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 of the Mach Number. 

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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