Computational Study on Compressor-Combustor Interactions for Improved Matching of a Micro Gas Turbine-Reference-Cited by-同舟云学术

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Computational Study on Compressor-Combustor Interactions for Improved Matching of a Micro Gas Turbine

Published:2024-02-29 Issue: Volume: Page:1-28
ISSN:0010-2202
Container-title:Combustion Science and Technology
language:en
Short-container-title:Combustion Science and Technology

Author:

Su Jingke¹,Liu Anxiong¹²,Luo Kun¹²,Liu Kai¹,Cheng Yuzhou²,Fan Jianren¹²

Affiliation:

1. College for Energy Engineering, Zhejiang University, Hangzhou, China

2. Shanghai Institute for Advanced Study, Zhejiang University, Shanghai, China

Funder

National Natural Science Foundation of China

Pujiang Talents Plan

Publisher

Informa UK Limited

Link

https://www.tandfonline.com/doi/pdf/10.1080/00102202.2024.2321972

Reference40 articles.

1. Hybrid RANS-LES Modeling of the Aerothermal Field in an Annular Hot Streak Generator for the Study of Combustor–Turbine Interaction

2. Towards the Large-Eddy Simulation of a full engine: Integration of a 360 azimuthal degrees fan, compressor and combustion chamber. Part I: Methodology and initialisation

3. Towards the Large-Eddy Simulation of a full engine: Integration of a 360 azimuthal degrees fan, compressor and combustion chamber. Part II: Comparison against stand-alone simulations

4. Modelling and simulation of gas turbines

5. Experimental Tests of the Operating Conditions of a Micro Gas Turbine Device

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