Advanced Compressible Flow Components Analysis
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.
Keywords: subsonic, Nozzle, Diffuser and Thrust analysis, compressible flow components, Mach Number
Linked Documents
Advanced Compressible Flow Components Analysis CE 2 Hour Quiz
Visited 974 times
$60.00
Related Courses
Compressible Flow Components Ideal vs Real Operation Analysis CE 1 Hour Quiz
Visited 1,165 times
$30.00
Compressible Flow Components Ideal vs Real Operation Analysis
Visited 2,250 times
$25.00
Buy This Course
Price :
$25.00 ( Per License )
Visited: 1965 Times
Difficulty: Normal
| # Licenses | Discounted Price |
| 1 | $25.00 |
| 10 | $23.75 |
| 25 | $23.13 |
| 50 | $22.50 |
| 100 | $21.25 |
| 100 | $21.25 |
| 100 | $21.25 |
Resold modules appear on your website. You earn syndication share from each purchase. Contact Coggno to learn more on how to embed your own Portable Webshop in your website.