Study on influence of admissions on loss generation in a twin-entry nozzleless radial turbine-Reference-Cited by-同舟云学术

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Study on influence of admissions on loss generation in a twin-entry nozzleless radial turbine

Published:2022-09 Issue: Volume:128 Page:107721
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wei Jiangshan,Yang Mingyang,Xue Yingxian,Deng Kangyao,Wang Cuicui,Wu Xintao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Radial turbine optimization under unsteady flow using nature-inspired algorithms;Mehrnia;Aerosp. Sci. Technol.,2020

2. Turbocharging: the Internal Combustion Engine;Watson,1982

3. Vaneless radial turbocharger turbine performance;Dale,1986

4. Performance of a twin-entry automotive turbocharger turbine;Capobianco,1993

5. Steady state performance evaluation of variable geometry twin-entry turbine;Romagnoli;Int. J. Heat Fluid Flow,2011

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A comparison study of loss generation between twin-entry and double-entry volutes of nozzled mixed-flow turbines;International Journal of Engine Research;2023-09-26

2. Numerical and experimental investigation of irreversible energy losses in a two-stage radial turbine under asymmetric inflow conditions;Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering;2023-03-25

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