Design optimization of the aerodynamic passive flow control on NACA 4415 airfoil using vortex generators
The present paper provides an experimental optimization of a NACA 4415 airfoil equipped
with vortex generators (VGs) to control its flow separation. To build this optimal configuration …
with vortex generators (VGs) to control its flow separation. To build this optimal configuration …
Microvortex generators in high-speed flow
A review of the state-of-the-knowledge of microvortex generators (MVGs) and their effect on
separated shock/boundary-layer interactions is provided. The flowfield around and behind …
separated shock/boundary-layer interactions is provided. The flowfield around and behind …
Investigation of pre-stall flow control on wind turbine blade airfoil using roughness element
In the current study, the aerodynamic performance of NACA 4412 airfoil with sandpaper
which was used as an alternative control device instead of vortex generators was …
which was used as an alternative control device instead of vortex generators was …
A review of the use of vortex generators for mitigating shock-induced separation
N Titchener, H Babinsky - Shock Waves, 2015 - Springer
This article reviews research into the potential of vortex generators to mitigate shock-
induced separation. Studies ranging from those conducted in the early post-war era to those …
induced separation. Studies ranging from those conducted in the early post-war era to those …
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 …
Unsteadiness in transonic shock-wave/boundary-layer interactions: experimental investigation and global stability analysis
A transonic interaction between a shock wave and a turbulent boundary layer is
experimentally and theoretically investigated. The configuration is a transonic channel flow …
experimentally and theoretically investigated. The configuration is a transonic channel flow …
Experimental and numerical investigation of the effects of passive vortex generators on Aludra UAV performance
A study of the effects of passive vortex generators (VGs) on Aludra unmanned aerial vehicle
(UAV) aerodynamic characteristics is presented. Both experimental and numerical works are …
(UAV) aerodynamic characteristics is presented. Both experimental and numerical works are …
Control of buffet phenomenon on a transonic swept wing
The control of the transonic buffet phenomenon over a half-model with a swept wing has
been investigated in the S3Ch wind tunnel of the ONERA Meudon center in the framework of …
been investigated in the S3Ch wind tunnel of the ONERA Meudon center in the framework of …
Shockwave/boundary-layer interaction control on a compression ramp using steady micro jets
SB Verma, C Manisankar - AIAA journal, 2012 - arc.aiaa.org
SHOCK-WAVE/BOUNDARY-LAYER interaction (SWBLI) in supersonic flow is initiated by
the strong adverse pressure gradient imposed by the interacting shock on the incoming …
the strong adverse pressure gradient imposed by the interacting shock on the incoming …
Separation and flow unsteadiness control in a compression corner induced interaction using mechanical vortex generators: Effects of vane size and inter-device …
SB Verma, C Manisankar - Physics of Fluids, 2022 - pubs.aip.org
An experimental investigation was conducted to control separation characteristics of a 24
compression corner induced interaction in a Mach 2.0 flow using an array of mechanical …
compression corner induced interaction in a Mach 2.0 flow using an array of mechanical …