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.
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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Compressible Flow Components Ideal vs Real Operation Analysis CE 1 Hour Quiz
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