Dynamics of three-dimensional shock-wave/boundary-layer interactions
DV Gaitonde, MC Adler - Annual Review of Fluid Mechanics, 2023 - annualreviews.org
Advances in measuring and understanding separated, nominally two-dimensional (2D)
shock-wave/turbulent-boundary-layer interactions (STBLI) have triggered recent campaigns …
shock-wave/turbulent-boundary-layer interactions (STBLI) have triggered recent campaigns …
Separation control with elliptical air-jet vortex generators
DP Ramaswamy, AM Schreyer - Experiments in Fluids, 2023 - Springer
The flow organisation of air-jet vortex generators (AJVGs) of elliptical cross sections and
their control effectiveness on a 24∘-compression-ramp-induced shock-wave/boundary-layer …
their control effectiveness on a 24∘-compression-ramp-induced shock-wave/boundary-layer …
Magnetic field control of high-enthalpy shock wave/boundary-layer interactions using a fully implicit thermochemical non-equilibrium solver
H Jiang, J Liu, X Che, Y Du, W Huang, F Ding… - Aerospace Science and …, 2023 - Elsevier
Magnetohydrodynamic (MHD) heat shield systems have been proven to be highly effective
in hypersonic blunt-nosed bodies. Thus, it is natural to consider the application of MHD to …
in hypersonic blunt-nosed bodies. Thus, it is natural to consider the application of MHD to …
Flow fields around asymmetrical micro vortex generators in supersonic flow
L Hristozova, R Sebastian, AM Schreyer - Aerospace Science and …, 2024 - Elsevier
Motivated by the favorable effects of asymmetrical vortical structures on shock-wave
boundary layer interactions, we performed implicit large-eddy simulations to analyze the …
boundary layer interactions, we performed implicit large-eddy simulations to analyze the …
Influence of crossflow Mach number on spanwise-inclined jet injection
R Sebastian, AM Schreyer - AIAA Scitech 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1363. vid Shock-wave/boundary-
layer interactions and associated flow separation are frequently occurring phenomena in …
layer interactions and associated flow separation are frequently occurring phenomena in …
[HTML][HTML] Design considerations for efficient spanwise-inclined air-jet vortex generators for separation control in supersonic and hypersonic flows
R Sebastian, AM Schreyer - Aerospace Science and Technology, 2024 - Elsevier
Shock-wave/boundary-layer interactions and associated flow separation are frequently
occurring phenomena in many high-speed flow applications. Injection of spanwise-inclined …
occurring phenomena in many high-speed flow applications. Injection of spanwise-inclined …
Influence of RVGA's height on suppressing the aero-optical effects induced by a supersonic mixing layer
Z Xia, H Ding, X Xu, S Yi - Applied Optics, 2022 - opg.optica.org
The supersonic mixing layer formed on the surface of hypersonic/supersonic flight vehicles'
optical windows is the main structure that induces aero-optical effects (AOEs), which may …
optical windows is the main structure that induces aero-optical effects (AOEs), which may …
基于Ramp-VG 阵列的超声速混合层流动控制实验研究
夏梓豪， 丁浩林， 易仕和， 孙明波 - 气体物理, 2022 - qtwl.xml-journal.net
利用基于纳米示踪的平面激光散射(nano-tracer-based planar laser scattering, NPLS)
技术研究了Ramp-VG 阵列对超声速混合层流场的控制效果. 对流Mach 数Ma c= 0.17 …
技术研究了Ramp-VG 阵列对超声速混合层流场的控制效果. 对流Mach 数Ma c= 0.17 …
超声速边界层气动光学效应及控制研究.
田立丰， 郭美琦， 丁浩， 黄开诱… - Journal of South China …, 2023 - search.ebscohost.com
光学成像制导技术是精确制导武器研究的重要课题, 气动光学效应的存在对制导精度产生严重的
影响, 使飞行器偏离目标位置, 甚至脱靶. 飞行器和来流之间的相互作用导致其周围流场结构非常 …
影响, 使飞行器偏离目标位置, 甚至脱靶. 飞行器和来流之间的相互作用导致其周围流场结构非常 …
Mach 3.5 Compression Corner Control Using Microvortex Generators
An experimental investigation has been performed to examine the effect of vortex generators
(VGs) on a compression corner flow separation. Experiments are conducted at Mach 3.5 …
(VGs) on a compression corner flow separation. Experiments are conducted at Mach 3.5 …