Study of the bow shock interaction with laser-pulse-heated air bubbles

E Schülein, A Zheltovodov, E Pimonov… - 39th AIAA Fluid …, 2009 - arc.aiaa.org
Flow control by energy deposition (ED) is the object of investigations at least since the
middle of the last century. Already the earlier experimental investigations1 show that, similar …

Laser energy deposition effectiveness on shock-wave boundary-layer interactions over cylinder-flare combinations

T Osuka, E Erdem, N Hasegawa, R Majima… - Physics of …, 2014 - pubs.aip.org
The effects of repetitive laser-pulse energy depositions (5.5 mJ/pulse) onto a shock wave-
boundary layer interaction region over cylinder-flare model in a Mach 1.92 flow are …

Quantification of the effect of surface heating on shock wave modification by a plasma actuator in a low-density supersonic flow over a flat plate

R Joussot, V Lago, JD Parisse - Experiments in Fluids, 2015 - Springer
This paper describes experimental and numerical investigations focused on the shock wave
modification induced by a dc glow discharge. The model is a flat plate in a Mach 2 air flow …

[HTML][HTML] Experimental investigation of expansion effect on shock wave boundary layer interaction near a compression ramp

HUO Junjie, YI Shihe, W Zheng, NIU Haibo… - Chinese Journal of …, 2022 - Elsevier
The experiment is conducted to investigate the effect of expansion on the shock wave
boundary layer interaction near a compression ramp. The small-angle expansion with an …

Influence of expansion waves on cowl shock/boundary layer interaction in hypersonic inlets

Y Zhang, H Tan, Y Zhuang, D Wang - Journal of Propulsion and Power, 2014 - arc.aiaa.org
The cowl shock/boundary layer interaction is of great importance to the performance and
operability of hypersonic inlets. However, it is usually affected by the expansion waves …

Simulation of NACA0015 flow separation control by burst-mode plasma actuation

B Wu, C Gao, F Liu, M Xue, B Zheng - Physics of Plasmas, 2019 - pubs.aip.org
Dielectric Barrier Discharge (DBD) plasma actuators can generate trains of vortices under
burst mode actuation, which is very different from the wall jet flow under steady operation. To …

Control mechanism of the three-dimensional shock wave/boundary layer interaction with the steady and pulsed micro-jets in a supersonic crossflow

Z Du, C Shen, W Huang, B Fan, Y Han - Physics of Fluids, 2022 - pubs.aip.org
The separation induced by shock wave/boundary layer interactions (SWBLI) is detrimental to
the performance of the flow field, and thus, needs to be reduced by using passive or active …

Investigation on the three-dimensional shock wave/turbulence boundary layer control induced by the secondary recirculation jets

Z Du, C Shen, W Huang, Y Shen, H Wu, Y Han - Computers & Fluids, 2022 - Elsevier
The interaction between the shock wave and the turbulence boundary layer induces a
separation, and this is an undesired phenomenon for the flow field performance. The control …

Suppression of reflected oblique shock wave by multi-filamentary plasma

SB Leonov, AA Firsov, AW Houpt - Journal of Physics …, 2018 - iopscience.iop.org
This paper describes the results of experimental study of stripwise near-surface plasma
effect on oblique shock wave (SW) reflection from a solid wall in a M= 2 duct-driven shock …

Flow structure generated by laser-induced blast wave propagation through the boundary layer of a flat plate

T Ukai, K Kontis, L Yang - Aerospace science and technology, 2018 - Elsevier
Laser energy deposition generates localized flow structures that can be used as flow control
devices in high-speed flows. In the present study, the interaction between a laser-induced …