The high-level objective of MARS project was to understand the formation and behaviour of turbulent structures which affects the Reynolds stress and skin friction. The aim was, once understood, to apply flow control techniques in order to control these structures and reduce the overall drag derived from the Reynolds stress and mainly from the skin friction. Active flow control devices were the main interest; DBD plasma, Synthetic jets, Micro Blowing and Suction, Moving Surfaces were included on the list. To test all these devices, two test cases were defined, and a database and file repository were established in the project webserver. The present chapter is aimed to describe the test cases, including the set-up of the flow control devices,...
The combination of landing future high mass systems with small landing footprints on Mars may requir...
From the signing of the Paris Agreement to the COVID-19 outbreak, the past decade has truly challeng...
In the context of building a framework for active flow control of turbulent boundary layers in wings...
The high-level objective of MARS project was to understand the formation and behaviour of turbulent ...
The focus of the present thesis is on the effects of two active flow control devices on the periodic...
This book includes a collection of chosen research papers from the partners of a research project (t...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76985/1/AIAA-2009-3918-290.pd
International audienceSince 1947, when Schubauer and Skramstad (J Res: 69–78, 1947 [1]) established ...
Skin friction drag reduction is one of the most promising paths in the investigation of the reductio...
This thesis shows the time-averaged effect of plasma and synthetic jet actuators on flow over bluff ...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revolution...
Several recent studies have shown the advantages of active and/or passive flow control devices for b...
A survey is made of recent computations published for synthetic jet flow control cases from a CFD wo...
Broad Flow Control Issues: a) Understanding flow physics. b) Specific control objective(s). c) Actua...
Turbulent flow separation over a wall-mounted hump model and its control using plasma actuators were...
The combination of landing future high mass systems with small landing footprints on Mars may requir...
From the signing of the Paris Agreement to the COVID-19 outbreak, the past decade has truly challeng...
In the context of building a framework for active flow control of turbulent boundary layers in wings...
The high-level objective of MARS project was to understand the formation and behaviour of turbulent ...
The focus of the present thesis is on the effects of two active flow control devices on the periodic...
This book includes a collection of chosen research papers from the partners of a research project (t...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76985/1/AIAA-2009-3918-290.pd
International audienceSince 1947, when Schubauer and Skramstad (J Res: 69–78, 1947 [1]) established ...
Skin friction drag reduction is one of the most promising paths in the investigation of the reductio...
This thesis shows the time-averaged effect of plasma and synthetic jet actuators on flow over bluff ...
Since 1947, when Schubauer and Skramstad established the basis of the technology with its revolution...
Several recent studies have shown the advantages of active and/or passive flow control devices for b...
A survey is made of recent computations published for synthetic jet flow control cases from a CFD wo...
Broad Flow Control Issues: a) Understanding flow physics. b) Specific control objective(s). c) Actua...
Turbulent flow separation over a wall-mounted hump model and its control using plasma actuators were...
The combination of landing future high mass systems with small landing footprints on Mars may requir...
From the signing of the Paris Agreement to the COVID-19 outbreak, the past decade has truly challeng...
In the context of building a framework for active flow control of turbulent boundary layers in wings...