Numerical analyses of heat transfer and thermal stress in a ZrB2 gas turbine stator blade

FS Moghanlou, M Vajdi, A Motallebzadeh, J Sha… - Ceramics …, 2019 - Elsevier
Temperature of burned gases is a key parameter in output works of gas turbines.
Nevertheless, high temperatures cause metallurgical problems in the turbine parts, specially …

Cost reduction for data acquisition based on data fusion: Reconstructing the surface temperature of a turbine blade

F Wen, Z Li, C Wan, L Su, Z Zhao, J Zeng, S Wang… - Physics of …, 2023 - pubs.aip.org
Turbine cooling is an effective way to improve the comprehensive performance and service
life of gas turbines. In recent decades, there has been rapid growth in research into external …

Определение локального коэффициента теплоотдачи с использованием модели температурного пограничного слоя с конвективной составляющей в …

АА Зуев, ВЮ Пиунов, ВП Назаров… - Вестник Южно …, 2019 - cyberleninka.ru
Учет особенностей теплоотдачи в проточных частях турбонасосных агрегатов (ТНА)
жидкостных ракетных двигателей (ЖРД) является важной задачей. Сопряженная …

Heat transfer, thermal stress and failure inspection of a gas turbine compressor stator blade made of five different conventional superalloys and ultra-high-temperature …

A Abid, MT Sarowar - Journal of Failure Analysis and Prevention, 2022 - Springer
Probing the efficiency of Brayton cycle is of great importance to harbor maximum output from
gas turbines. The efficiency of Brayton cycle largely depends on the maximum temperature …

Effect of non-axisymmetric endwall and periodic upstream wakes on the aero-thermal dynamics in turbine cascade

C Hu, H Liu, K Geng, C Yang - International Journal of Mechanical …, 2021 - Elsevier
The thermal management and heat transfer behavior considering both the contoured
endwall and upstream wakes were seldom investigated. In the present work, the …

Effect of shelf squealer tip configuration on aerothermal performance of gas turbine blade

JJ Kim, W Seo, H Chung, M Bang, HH Cho - International Journal of …, 2021 - Elsevier
The tip leakage flow between rotating turbine blades and the stationary turbine casing
causes aerodynamic losses and high thermal loads. Numerous novel tip geometries have …

Geometric nonlinear vibrations of rotating variable thickness plates induced by periodic incoming wakes

H Kou, T Zhao, J Du, L Zeng, Z Zhu, F Zhang… - International Journal of …, 2020 - Elsevier
Incoming wakes significantly affect vibration characteristics of rotating blades in
turbomachines. This paper develops a periodic incoming wake mathematical model to …

Effects of varying non-axisymmetric contours of the turbine endwall on aerodynamics and heat transfer Aspects: A sensitivity analysis study

P Chen, K Zhao, X Li, J Ren, H Jiang - International Journal of Thermal …, 2021 - Elsevier
Non-axisymmetric endwall contouring of gas turbines has been widely employed as an
effective way to improve the aerodynamic performance or heat transfer features. Though …

Innovative Framework for Robustness Analysis of Blade Multicavity Squealer Tip Aerothermal Performance

M Huang, K Zhang, Z Li, J Li - Journal of Thermophysics and Heat …, 2024 - arc.aiaa.org
Gas turbines are subject to various geometric and operational uncertainties, which are often
overlooked in conventional research. Therefore, conclusions derived from a deterministic …

Multi-fidelity surrogate models for predicting averaged heat transfer coefficients on endwall of turbine blades

W Choi, K Radhakrishnan, NH Kim, JS Park - Energies, 2021 - mdpi.com
This paper proposes a multi-fidelity surrogate (MFS) model for predicting the heat transfer
coefficient (HTC) on the turbine blades. First, the low-fidelity (LF) and high-fidelity (HF) …