This report summarizes the design optimizations of several concepts of high-lift systems for laminar wing airfoils. The airfoil wing section used is the airfoil shape denoted LV1 taken form the laminar airfoil catalogue. The design was performed in a 2D normalized manner. Three concepts were investigated, one at the leading edge and two at the trailing edge. The designed high-lift concepts show suitable aerodynamic performance for the realisation of laminar wing technology at high-lift conditions
Experiments were performed on a slotted natural laminar flow airfoil, the S414. The slotted natural ...
The scope of the paper is to present the results of a RANS-based aerodynamic high-lift design for a ...
The scope of the paper is to present the results of a RANS-based aerodynamic high-lift design for a ...
The paper describes the aerodynamic design of a high lift system suitable for a Natural Laminar Flow...
The presentation summarizes the design of high-lift devices for laminar wings. Within the EC-project...
The presenatation summarizes teh design of high-lift devices for laminar wings. Within the EC projec...
This article describes the design and optimization of a high-lift system for a forward swept wing in...
The paper deals with the aerodynamic design of laminar flow wings. The main concepts at present appl...
A novel high Reynolds number design for airfoils with an application in the outer part of a modern t...
The design of high-lift (HL) systems represents a challenging task within the aerospace community, d...
The design of high-lift (HL) systems represents a challenging task within the aerospace community, d...
Abstract. The design of high-lift (HL) systems represents a challenging task within the aero-space c...
In the present work, the aerodynamic shape design of an advanced high-lift system for a natural lami...
The EUROLIFT II project, funded by the European Commission within the 6th framework programme, is de...
The scope of the paper is to present the results of a RANS based aerodynamic high-lift design for a ...
Experiments were performed on a slotted natural laminar flow airfoil, the S414. The slotted natural ...
The scope of the paper is to present the results of a RANS-based aerodynamic high-lift design for a ...
The scope of the paper is to present the results of a RANS-based aerodynamic high-lift design for a ...
The paper describes the aerodynamic design of a high lift system suitable for a Natural Laminar Flow...
The presentation summarizes the design of high-lift devices for laminar wings. Within the EC-project...
The presenatation summarizes teh design of high-lift devices for laminar wings. Within the EC projec...
This article describes the design and optimization of a high-lift system for a forward swept wing in...
The paper deals with the aerodynamic design of laminar flow wings. The main concepts at present appl...
A novel high Reynolds number design for airfoils with an application in the outer part of a modern t...
The design of high-lift (HL) systems represents a challenging task within the aerospace community, d...
The design of high-lift (HL) systems represents a challenging task within the aerospace community, d...
Abstract. The design of high-lift (HL) systems represents a challenging task within the aero-space c...
In the present work, the aerodynamic shape design of an advanced high-lift system for a natural lami...
The EUROLIFT II project, funded by the European Commission within the 6th framework programme, is de...
The scope of the paper is to present the results of a RANS based aerodynamic high-lift design for a ...
Experiments were performed on a slotted natural laminar flow airfoil, the S414. The slotted natural ...
The scope of the paper is to present the results of a RANS-based aerodynamic high-lift design for a ...
The scope of the paper is to present the results of a RANS-based aerodynamic high-lift design for a ...