Compressible Flow Components Analysis

Created by: Engineering Software
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Last Updated 01/2026
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What you'll learn

In this course, the student gets familiar with the compressible flow components and their T - s diagrams
Ideal operation and major performance trends

Amendment 42-24 Authorized for use 1 January 2025 / Mandatory 1 January 2026

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.

Table of Contents

Nozzle
Analysis
Assumptions
Governing Equations
Input Data
Results
Conclusions
Diffuser
Analysis
Assumptions
Governing Equations
Input Data
Results
Conclusions
Thrust
Analysis
Assumptions
Governing Equations
Input Data
Results
Conclusions

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