Advanced Compressible Flow Components AnalysisAuthor: Gordan Feric
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.
In this course material, the student gets familiar with the compressible flow components (nozzle, diffuser and thrust) and their T - s diagrams, operation and major performance trends.
Buy This Course
$25.00 ( Per License )
Visited: 1870 Times
|# Licenses||Discounted Price|