[HTML][HTML] Micro gas turbine: Developments, applications, and key technologies on components

J Li, Y Li - Propulsion and Power Research, 2023 - Elsevier
Owing to their precedent characteristics, micro gas turbines (MGTs) have been favored as
popular power machinery in plenty of energy systems such as distributed energy systems …

Thermo-hydraulic performance optimization of a disk-shaped microchannel heat sink applying computational fluid dynamics, artificial neural network, and response …

K Vaferi, M Vajdi, S Nekahi, A Heydari, FS Moghanlou… - Heliyon, 2023 - cell.com
The current research focuses on optimizing the Nusselt number (Nu) and pressure drop (ΔP)
in a bionic fractal heat sink. The artificial neural network (ANN) and response surface …

Comparative study of four displacer phase-shifters in a split pulse tube refrigerator working at 170 K

P Zheng, X Chen, Y Wu, W Duan, H Zhang - Applied Thermal Engineering, 2023 - Elsevier
A pulse tube refrigerator (PTR) with a displacer phase-shifter has great potential for realizing
high-efficiency PTRs. There are four types of displacer phase-shifters: passive rod displacer …

[HTML][HTML] Performance of insulators under variation of pollution, inclined angle, and temperature based on the design of experiment

RNR Ghaly, SSM Ghoneim, A Ibrahim, W Ziomek… - Results in …, 2024 - Elsevier
The environmental conditions significantly impact the performance of the transmission line
insulators. The current work investigated some variables that influence the flashover and …

Combustion and particulate I/SVOC characteristics of an aero-engine combustor with dual-stage under operational power and injection pressure

Z Liang, H Liu, Z Han, Y Fan, L Lei - Energy, 2024 - Elsevier
The combustion and particulate intermediate-volatile/semi-volatile organic compound
(I/SVOC) emission characteristics of a technology of low emission stirred swirl aero-engine …

[HTML][HTML] Evaluation of machine learning models for predicting performance metrics of aero-engine combustors

H Yang, S Guo, H Xie, J Wen, J Wang - Case Studies in Thermal …, 2025 - Elsevier
As environmental standards tighten and aero-engine performance improves, credible
mapping between structural parameters and performance metrics is crucial for optimizing …

Heat Transfer Characteristics of an Aeroengine Turbine Casing Based on CFD and the Surrogate Model

W Lian, Y Jiang, H Chen, Y Li, X Liu - Energies, 2022 - mdpi.com
A good turbine casing cooling design should control the thermal stress and maintain a
reasonable tip clearance between the turbine blade and the casing. Since the turbine inlet …

作战仿真混合实验方案设计研究

刘飞, 赖鹏, 陆营波, 汪敏, 陆志沣 - 系统仿真学报, 2024 - china-simulation.com
作战仿真实验方案设计指的是基于基准的作战想定, 利用各种实验设计方法对实验因子的取值
进行抽样, 形成一组实验方案, 供后续仿真使用. 作战仿真的复杂性包括实验因子数目众多 …

[PDF][PDF] Numerical Simulation of H2 Addition Effect to CH4 Premixed Turbulent Flames for Gas Turbine Burner

S Ouali - Journal of Applied Fluid Mechanics, 2024 - researchgate.net
Present computational simulation studied H2-CH4 combustion characteristics in a specific
gas turbine combustor used for power generation. Across four thermal loads (1.1-4.4 bar) …

Comparison of Response Surface-Based Preliminary Design Methodologies for a Gas Turbine Combustor.

N Mahto, SR Chakravarthy - Defence Science Journal, 2024 - search.ebscohost.com
The preliminary design of gas turbine combustors is a multi-objective optimization problem.
The methodology to be used at the preliminary design stage depends on the freedom of …