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Created by Gordan Feric
Category Engineering > Other
The 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 ofthe Mach Number and isentropic nozzle and diffuser efficiency.
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), their T - s diagrams, ideal vs real operation and major performance trends.
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
Understand basic energy conversion engineering assumptions and equations
Know basic elements of the Brayton Cycle, Otto Cycle, Diesel Cycle, compression, combustion and expansion processes and their T -s, p-V and h-T diagrams.
Be familiar with Brayton Cycle, Otto Cycle, Diesel Cycle, compression, combustion and expansion ideal vs real operation
Understand general Brayton Cycle, Otto Cycle, Diesel Cycle, compression, combustion and expansion performance trends.
English
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by Gordan Feric
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by Gordan Feric
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