Aerothermodynamic similarity criteria for turbines operating within non-periodic transition processes
Author:
Funder
National Natural Science Foundation of China
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Reference26 articles.
1. Axial Turbine Aerodynamics for Aero-Engines: Flow Analysis and Aerodynamics Design;Zou,2018
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3. Gas turbine engine transient performance and heat transfer effect modelling: a comprehensive review, research challenges, and exploring the future;Yang;Appl. Therm. Eng.,2024
4. Predicting efficiency of a turbine driven by pulsating flow;Fernelius,2017
5. Thermodynamic analysis of a gas turbine engine with a rotating detonation combustor;Sousa;Appl Energy,2017
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