Brayton Cycle (Gas Turbine) Ideal vs Real Operation for Propulsion Application Analysis
1h! Run Time
Employees
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Supervisors
Provided
What you'll learn
Skills covered in this course
Description
In this course material, the open, simple Brayton Cycle used for stationary power generation is considered providing thrust instead of power output. To keep the scope of the thrust analysis simple, the working fluid exiting the gas turbine expands to atmospheric conditions, so the final working fluid exit pressure is equal to the ambient pressure.
What this course covers:
- Brayton Cycle thermal efficiency presented for air as the working fluid, with the derivation shown using a simple mathematical approach.
- The Brayton Cycle represented on a T-s diagram.
- Major performance trends (specific propulsion output and propulsion output) plotted as functions of compression ratio, gas turbine inlet temperature, working fluid mass flow rate, and both isentropic compression and expansion efficiency.
Note that this course material does not deal with costs (capital, operational or maintenance).
Table of Contents
Brayton Cycle (Gas Turbine) for Propulsion Application
Analysis
Assumptions
Governing Equations
Input Data
Results
Conclusions
System Requirements
See System Requirements in the Coggno Knowledge Base