Compressible Flow Components Ideal vs Real Operation Analysis

Author: Gordan Feric

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.

In this course material, the student gets familiar with the compressible flow components (nozzle, diffuser and thrust), their T - s diagrams, ideal vs real operation and major performance trends.

Keywords: Nozzle, Diffuser and Thrust Ideal vs Real Operation, compressible flow components, Mach Number, isentropic

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