Description
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.
What you'll learn
In this course, the student gets familiar with the compressible flow components (nozzle, diffuser and thrust), their T - s diagrams, operation and major performance trends.
Gordan Feric
His over 25 years engineering experience includes performing analytical modeling and computer modeling of physical properties, power cycles, power cycle components/processes and compressible flow. Also, conducting conceptual design, analysis and evaluation of energy conversion systems for basic and simple power and propulsion cycles.