This course has been discontinued.
The ideal 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 of the Mach Number.
This interactive online course 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, you will become familiar with the compressible flow components (nozzle, diffuser and thrust), their T - s diagrams, operation and major performance trends.