Conjugate heat transfer analysis on return-flow impingement cooling scheme applied to aeroengine turbine blade leading edge

作者：Han Yan, Lei Luo, Yue Li, Yufan Wang, Wei Du, Licheng Guo · 发表于：Aerospace Science and Technology · 年份：2025 · DOI：10.1016/j.ast.2025.110604 · 被引用次数：11 · 研究领域：Heat Transfer Mechanisms、Turbomachinery Performance and Optimization、Heat transfer and supercritical fluids