Add to ORKGThe present paper deals with the control of the laminar-turbulent transition on a swept wing in supersonic conditions. This study has been carried out as part of the European Project SUPERTRAC (SUPERsonic TRAnsition Control; January 2005, June 2008). Two issues have been addressed with the same model: the first one is the control of the transition due to crossflow (CF) instabilities present on a swept wing, by using Micron-Sized Roughness elements (MSR); the second one is the prevention of the turbulent contamination along the leading edge by means of appropriate Anti-Contamination Devices (ACD). The paper describes the work concerning the numerical approach, the model design, the tests in the ONERA S2MA wind tunnel in Modane and the an...
The market growth expected for commercial aviation in the coming decades and the increasing social a...
A study of the laminar/turbulent transition have been conducted at the Institute of Design Aerodynam...
A parametric study to predict the extent of laminar flow on the upper surface of a generic swept-bac...
This paper presents an attempt to control the laminar-turbulent transition on a swept wing in supers...
This paper presents an attempt to control the laminar-turbulent transition on a swept wing in supers...
The global objective of the SUPERTRAC project is to explore the possibilities to delay laminar-turbu...
The global objective of the SUPERTRAC project is to explore the possibilities to delay laminar-turbu...
Different concepts of laminar flow control for supersonic swept wing flows are currently investiga...
The supersonic aircraft transport is still a challenge for the aeronautical scientific com-munity. I...
Key words: swept wing, supersonic boundary layer, cross flow instability, laminar- turbulent transit...
The experimental results of the investigations of the transition-delay on a supersonic swept wing by...
The work contained in this report is concerned with the use of transpiration at the leading edge of ...
For subsonic and transonic flight Mach numbers the feasibility and potential benefits of laminar flo...
The represented paper is a brief overview of some activities in laminar flow control area being perf...
Laminarization of wetted surfaces on subsonic/transonic transport aircraft is one of the big challen...
The market growth expected for commercial aviation in the coming decades and the increasing social a...
A study of the laminar/turbulent transition have been conducted at the Institute of Design Aerodynam...
A parametric study to predict the extent of laminar flow on the upper surface of a generic swept-bac...
This paper presents an attempt to control the laminar-turbulent transition on a swept wing in supers...
This paper presents an attempt to control the laminar-turbulent transition on a swept wing in supers...
The global objective of the SUPERTRAC project is to explore the possibilities to delay laminar-turbu...
The global objective of the SUPERTRAC project is to explore the possibilities to delay laminar-turbu...
Different concepts of laminar flow control for supersonic swept wing flows are currently investiga...
The supersonic aircraft transport is still a challenge for the aeronautical scientific com-munity. I...
Key words: swept wing, supersonic boundary layer, cross flow instability, laminar- turbulent transit...
The experimental results of the investigations of the transition-delay on a supersonic swept wing by...
The work contained in this report is concerned with the use of transpiration at the leading edge of ...
For subsonic and transonic flight Mach numbers the feasibility and potential benefits of laminar flo...
The represented paper is a brief overview of some activities in laminar flow control area being perf...
Laminarization of wetted surfaces on subsonic/transonic transport aircraft is one of the big challen...
The market growth expected for commercial aviation in the coming decades and the increasing social a...
A study of the laminar/turbulent transition have been conducted at the Institute of Design Aerodynam...
A parametric study to predict the extent of laminar flow on the upper surface of a generic swept-bac...