Comprehensive investigations on fluid flow and heat transfer characteristics of a high-speed rotating turbine disk cavity system of aero-engine-Reference-Cited by-同舟云学术

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Comprehensive investigations on fluid flow and heat transfer characteristics of a high-speed rotating turbine disk cavity system of aero-engine

Published:2022-07 Issue: Volume:136 Page:106170
ISSN:0735-1933
Container-title:International Communications in Heat and Mass Transfer
language:en
Short-container-title:International Communications in Heat and Mass Transfer

Author:

Lin Aqiang,Liu Gaowen,Yu Xiangxian,Chang Ran,Feng Qing

Funder

National Major Science and Technology Projects of China

Basic and Applied Basic Research Foundation of Guangdong Province

Northwestern Polytechnical University

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

Condensed Matter Physics,General Chemical Engineering,Atomic and Molecular Physics, and Optics

Reference38 articles.

1. Development of key technologies for the next generation gas turbine;Ito,2007

2. Theoretical and experimental evaluation of temperature drop and power consumption in a cover-plate pre-swirl system for gas turbine cooling;Liu;Case Stud. Thermal Eng.,2021

3. Gas turbine heat transfer: ten remaining hot gas path challenges;Bunker;J. Turbomach.,2007

4. Prediction of the sealing flow effect on the temperature drop characteristics of a pre-swirl system in an aero-engine;Liu;Appl. Therm. Eng.,2021

5. Evaluation of thermal management strategy based on zoning of stress states of a gas turbine disk;Li;Int. Communicat. Heat Mass Transfer,2017

Cited by 17 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. Optimizing heat transfer predictions in HCNG engines: A novel model validation and comparative study via quasi-dimensional combustion modeling and artificial neural networks;International Journal of Hydrogen Energy;2024-09

2. Experimental investigations of aero-engine pre-swirl system performance improvement with consideration of inner seal flow effect;Physics of Fluids;2024-08-01

3. Torque and energy recovery of a compressor disk cavity in gas turbine engines;Case Studies in Thermal Engineering;2024-08

4. The effect of rotor roughness on flow and heat transfer in rotor–stator cavities with different axial gap;Applied Thermal Engineering;2024-08

5. Investigations of a turbine pre-swirl system with high temperature drop efficiency through the design of a novel vane-shaped receiver hole;Energy;2024-08

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