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Hypersonic transition induced by three isolated roughness elements on a flat plate
Zhiwei Duan, Zhixiang Xiao
Tsinghua University
来源Computers & Fluids
年份2017
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学术脉络
学科主题
工程Fluid Dynamics and Turbulent Flows
Computational Fluid Dynamics and Aerodynamics · Gas Dynamics and Kinetic Theory
参考文献 21
Flow-field and drag characteristics of several boundary-layer tripping elements in hypersonic flow
被引 32A. H. Whitehead · NASA Technical Reports Server (NASA) · 1969
Numerical simulations of hypersonic boundary layer transition.
被引 20Matthew Bartkowicz · University of Minnesota Digital Conservancy (University of Minnesota) · 2012
Boundary-Layer Transition at Supersonic Speeds - Three-Dimensional Roughness Effects (Spheres)
被引 72E. R. Van Driest · Journal of the aerospace sciences/Journal of the aero/space sciences · 1962
此处列出前 3 条
引用本文 22
Direct numerical simulation of high-speed transition due to roughness elements
被引 40Prakash Shrestha, Graham V. Candler · Journal of Fluid Mechanics · 2019
First-mode-induced nonlinear breakdown in a hypersonic boundary layer
被引 28Sasidharan Nair Unnikrishnan, Datta V. Gaitonde · Computers & Fluids · 2019
Effect of three-dimensional smooth humps on hypersonic boundary layer instability of streamwise vortices over a yawed cone
被引 9Xiaohu Li, Qiang Yang, Jianqiang Chen · Physics of Fluids · 2021
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