Study of design methods and heat transfer characteristics of combined cooling structure for turbine blades with turbine inter-vane burner-Reference-Cited by-同舟云学术

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Study of design methods and heat transfer characteristics of combined cooling structure for turbine blades with turbine inter-vane burner

Published:2024-10 Issue: Volume:254 Page:123866
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Cheng Zeyuan,Zhang Heng,Qing Liming,Zhu Jianqin^ORCID

Funder

National Major Science and Technology Projects of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference35 articles.

1. Numerical Analysis of Inter-Turbine Burner (ITB) Concepts for Improved Gas Turbine Engine Performance;Mawid,2005

2. A review of gas turbine engine with inter-stage turbine burner;Yin;Prog. Aerosp. Sci.,2020

3. Ultra-compact combustion technology using high swirl for enhanced burning rate;Zelina;Aiaa/asme/sae/asee Joint Propulsion Conference & Exhibit.,2002

4. Reacting mixing-layer computations in a simulated turbine-stator passage;Cheng;J. Propul. Power,2009

5. A review of cooling technologies for high temperature rotating components in gas turbine;Unnikrishnan;Propul. Power Res.,2022

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