The Law of the Total Pressure Loss in Supersonic Streamwise Corner Flow

被引：0
|
作者：
Yang, Rui [1 ]
Jin, Jiahui [1 ]
Zhao, Yuxin [1 ]
机构：
[1] National University of Defence Technology, Hunan, Changsha,410073, China
来源：
Journal of Physics: Conference Series | 2024年 / 2860卷 / 01期
关键词：
Compilation and indexing terms; Copyright 2025 Elsevier Inc;
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学科分类号：
摘要：
Boundary layer flow - Channel flow - Compressibility - Compressible flow - Hydraulics - Hypersonic boundary layers - Hypersonic flow - Hypersonic vehicles - Pressure effects - Secondary flow - Supersonic aircraft - Supersonic flow
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