3. Conclusion
Optimum turbomachinery efficiency is an imperative for both theoretical and experimental research, and all the more so as these machines are coupled in thermodynamic cycles. To conclude, let's take the example of a gas turbine comprising an adiabatic compressor, a constant-pressure combustor and an adiabatic turbine coupled to the compressor. Figure
21
shows the efficiency of this gas turbine operating between the extreme temperatures of 15°C (upstream compressor) and 1000°C (upstream turbine).
Exclusive to subscribers. 97% yet to be discovered!
Already subscribed? Log in!
Conclusion
Glossary
Article included in this offer
"Hydraulic, aerodynamic and thermal machines"
(
177 articles
)
Updated and enriched with articles validated by our scientific committees
A set of exclusive tools to complement the resources
Bibliography
Exclusive to subscribers. 97% yet to be discovered!
Already subscribed? Log in!
