Simulation study on the flow characteristic and combustion performance in a high-temperature rise combustor based on RQL under different length of quench zone
Author:
Funder
National Natural Science Foundation of China
Natural Science Foundation of Guizhou Province
Scientific Research Project of Higher Education Institutions of Guizhou Province
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s40430-024-04989-6.pdf
Reference24 articles.
1. Zeng Q, Chen X (2023) Combustor technology of high temperature rise for aero engine. Prog Aerosp Sci 140:100927
2. Wang KF, Li F, Zhou T et al (2024) Numerical simulations on the effect of swirler installation angle on outlet temperature distribution. Appl Therm Eng 240:12252
3. Mongia H (2011) Engineering aspects of complex gas turbine combustion mixers part I: high ΔT. In: 49th AIAA aerospace science meeting including the new horizons forum and aerospace exposition, Orlando, Florida
4. Mongia H (2011) Engineering aspects of complex gas turbine combustion mixers part II: high T3. In: 49th AIAA aerospace science meeting including the new horizons forum and aerospace exposition, Orlando, Florida
5. Mongia H (2011) Engineering aspects of complex gas turbine combustion mixers part III: 30 OPR. In: 9th Annual international energy conversion engineering conference, San Diego, California
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