Study of the streamwise location of a micro vortex generator for a separation-control mechanism in supersonic flow
H Wu, W Huang, XY Zhong, ZB Du - Physics of Fluids, 2022 - pubs.aip.org
A shock wave/boundary layer interaction is a common phenomenon in supersonic
(hypersonic) flows, and it usually occurs in an airbreathing propulsion system. It induces a …
(hypersonic) flows, and it usually occurs in an airbreathing propulsion system. It induces a …
Numerical investigation and optimization on the micro-ramp vortex generator within scramjet combustors with the transverse hydrogen jet
L Li, W Huang, L Yan, Z Du, M Fang - Aerospace Science and Technology, 2019 - Elsevier
An effective fuel supply strategy with high mixing efficiency, large penetration depth and low
stagnation pressure losses determines the overall performance of the scramjet (supersonic …
stagnation pressure losses determines the overall performance of the scramjet (supersonic …
[PDF][PDF] Micro vortex generators for boundary layer control: principles and applications
Z Sun - International Journal of Flow Control, 2015 - openaccess.city.ac.uk
A review is given to the major developments in the boundary layer control by means of micro
vortex generator (MVG). The appearance of MVG dates back to about three decades from …
vortex generator (MVG). The appearance of MVG dates back to about three decades from …
Normal shock boundary layer control with various vortex generator geometries
Various vortex generators which include ramp, split-ramp and a new hybrid concept
“ramped-vane” are investigated under normal shock conditions with a diffuser at Mach …
“ramped-vane” are investigated under normal shock conditions with a diffuser at Mach …
Traditional and new types of passive flow control techniques to pave the way for high maneuverability and low structural weight for UAVs and MAVs
Prevailing utilization of airfoils in the design of micro air vehicles and wind turbines causes
to gain attention in terms of determination of flow characterization on these flight vehicles …
to gain attention in terms of determination of flow characterization on these flight vehicles …
Effect of air jet vortex generators on a shock wave boundary layer interaction
LJ Souverein, JF Debiève - Experiments in Fluids, 2010 - Springer
The effect of upstream injection by means of continuous air jet vortex generators (AJVGs) on
a shock wave turbulent boundary layer interaction is experimentally investigated. The …
a shock wave turbulent boundary layer interaction is experimentally investigated. The …
Direct numerical simulation of supersonic boundary layers over a microramp: effect of the Reynolds number
Microvortex generators are passive control devices smaller than the boundary layer
thickness that energise the boundary layer to prevent flow separation with limited induced …
thickness that energise the boundary layer to prevent flow separation with limited induced …
The three-dimensional flow organization past a micro-ramp in a supersonic boundary layer
The three-dimensional instantaneous flow organization in the near wake of a micro-ramp
interacting with a Mach 2.0 supersonic turbulent boundary layer is studied using …
interacting with a Mach 2.0 supersonic turbulent boundary layer is studied using …
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 …
Numerical study of micro-ramp vortex generator for supersonic ramp flow control at Mach 2.5
An implicit large eddy simulation, implemented using a fifth-order, bandwidth-optimized
weighted essentially non-oscillatory scheme, was used to study the flow past a compression …
weighted essentially non-oscillatory scheme, was used to study the flow past a compression …