Transition and turbulence production in a hypersonic boundary layer is investigated in the Mach 6 wind tunnel at Peking University, using Rayleigh-scattering visualization, fast-response pressure measurements, and particle image velocimetry. Detailed analysis of the experimental observations is provided. It is found that, although the second mode is primarily an acoustic wave, it causes the formation of high-frequency vortical waves. Moreover, the second mode interacts strongly with low-frequency waves, which leads to immediate transition to turbulence.National Natural Science Funds of China [10921202, 11221061, 11521091]SCI(E)EIARTICLEzhuhope@126.com; zch58@163.com; chenxicoe@pku.edu.cn; yuanhj@pku.edu.cn; jzwu@coe.pku.edu.cn; sycpku@163...
Hypersonics is of current national interest, but improved understanding of fundamental flow physics ...
The evolution of Görtler vortices and its interaction with other instabilities are investigated in t...
This project is based on Dr. Duan’s proposal, titled “Numerical Simulation of Freestream Acoustic Di...
Transition and turbulence production in a hypersonic boundary layer is investigated in a Mach 6 wind...
Transition on a flared cone with zero angle of attack was studied in our newly established Mach 6 qu...
Transition from laminar to turbulent flow in hypersonic boundary layers leads to highly elevated lev...
During atmospheric reentry, hypersonic vehicles are subjected to high levels of boundary-layer press...
During atmospheric reentry, hypersonic vehicles are subjected to high levels of boundary-layer press...
Hypersonic boundary-layer transition can be caused by many different mechanisms. This research focus...
The excitation of instability modes in the wake generated behind a discrete roughness element in a b...
In this research, to study the hypersonic boundary-layer transition, experiments were conducted on a...
Boundary layer receptivity to two-dimensional acoustic disturbances at different incidence angles an...
High speed flow visualization,wall pressure measurement and PIV were used to study the transition of...
Direct Numerical Simulations (DNS) were carried out to investigate the laminar-turbulent transition ...
Transition from laminar to turbulent hypersonic boundary layers is the topic of several research pro...
Hypersonics is of current national interest, but improved understanding of fundamental flow physics ...
The evolution of Görtler vortices and its interaction with other instabilities are investigated in t...
This project is based on Dr. Duan’s proposal, titled “Numerical Simulation of Freestream Acoustic Di...
Transition and turbulence production in a hypersonic boundary layer is investigated in a Mach 6 wind...
Transition on a flared cone with zero angle of attack was studied in our newly established Mach 6 qu...
Transition from laminar to turbulent flow in hypersonic boundary layers leads to highly elevated lev...
During atmospheric reentry, hypersonic vehicles are subjected to high levels of boundary-layer press...
During atmospheric reentry, hypersonic vehicles are subjected to high levels of boundary-layer press...
Hypersonic boundary-layer transition can be caused by many different mechanisms. This research focus...
The excitation of instability modes in the wake generated behind a discrete roughness element in a b...
In this research, to study the hypersonic boundary-layer transition, experiments were conducted on a...
Boundary layer receptivity to two-dimensional acoustic disturbances at different incidence angles an...
High speed flow visualization,wall pressure measurement and PIV were used to study the transition of...
Direct Numerical Simulations (DNS) were carried out to investigate the laminar-turbulent transition ...
Transition from laminar to turbulent hypersonic boundary layers is the topic of several research pro...
Hypersonics is of current national interest, but improved understanding of fundamental flow physics ...
The evolution of Görtler vortices and its interaction with other instabilities are investigated in t...
This project is based on Dr. Duan’s proposal, titled “Numerical Simulation of Freestream Acoustic Di...