Research progress of hypersonic boundary layer transition control experiments
H Yang, H Liang, S Guo, M Tang, C Zhang… - Advances in …, 2022 - Springer
Hypersonic boundary layer transition is a hot yet challenging problem restricting the
development and breakthrough of hypersonic aerodynamics. In recent years, despite great …
development and breakthrough of hypersonic aerodynamics. In recent years, despite great …
Observations of hypervelocity boundary-layer instability
A novel optical method is used to measure the high-frequency (up to 3 MHz) density
fluctuations that precede transition to turbulence within a laminar boundary layer in a …
fluctuations that precede transition to turbulence within a laminar boundary layer in a …
Differential interferometric measurement of instability in a hypervelocity boundary layer
THE prediction of laminar–turbulent transition location in high-speed boundary layers is
critical to hypersonic vehicle design because of the weight implications of increased skin …
critical to hypersonic vehicle design because of the weight implications of increased skin …
[HTML][HTML] 高超声速边界层转捩实验综述
刘向宏， 赖光伟， 吴杰 - 空气动力学学报, 2018 - html.rhhz.net
高超声速边界层转捩直接影响飞行器表面的摩擦系数与热流分布, 对于高超声速飞行器的气动
布局以及热防护设计至关重要. 尽管高超声速边界层层/湍流转捩的相关研究已经开展长达半个 …
布局以及热防护设计至关重要. 尽管高超声速边界层层/湍流转捩的相关研究已经开展长达半个 …
[图书][B] Slender-body hypervelocity boundary-layer instability
N Parziale - 2013 - search.proquest.com
With novel application of optical techniques, the slender-body hypervelocity boundary-layer
instability is characterized in the previously unexplored regime where thermo-chemical …
instability is characterized in the previously unexplored regime where thermo-chemical …
[HTML][HTML] Attenuation of hypersonic second-mode boundary-layer instability with an ultrasonically absorptive silicon-carbide foam
Unsteady surface pressure measurements have been carried out on a flat-plate test article in
the Air Force Research Laboratory's Mach-6 Ludwieg Tube at a negative angle of attack …
the Air Force Research Laboratory's Mach-6 Ludwieg Tube at a negative angle of attack …
[HTML][HTML] Unsteady heat-flux measurements of second-mode instability waves in a hypersonic flat-plate boundary layer
MA Kegerise, SJ Rufer - Experiments in fluids, 2016 - Springer
In this paper, we report on the application of the atomic layer thermopile (ALTP) heat-flux
sensor to the measurement of laminar-to-turbulent transition in a hypersonic flat-plate …
sensor to the measurement of laminar-to-turbulent transition in a hypersonic flat-plate …
Time-resolved visualization of instability waves in a hypersonic boundary layer
SJ Laurence, A Wagner, K Hannemann, V Wartemann… - AIAA journal, 2012 - arc.aiaa.org
LAMINAR–TURBULENT transition in hypersonic boundary layers remains a challenging
subject. This is especially true of the hypervelocity regime, in which an intriguing …
subject. This is especially true of the hypervelocity regime, in which an intriguing …
Identification of traveling crossflow waves under real hypersonic flight conditions
B Wan, G Tu, X Yuan, J Chen, Y Zhang - Physics of Fluids, 2021 - pubs.aip.org
Understanding crossflow instabilities in three-dimensional boundary layers triggered by
either traveling crossflow waves or stationary crossflow vortices is of great importance for …
either traveling crossflow waves or stationary crossflow vortices is of great importance for …
Ultrasonically absorptive silicon-carbide foam for boundary-layer control
BL Bemis, JL Brun, CT Wanstall, JL Hill… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0096. vid Unsteady surface
pressure measurements have been carried out on a flat-plate test article in the Air Force …
pressure measurements have been carried out on a flat-plate test article in the Air Force …