The main aim of the present paper is to investigate the influence of multiple winglets on hang-glider climbing performance. The study aims to optimize the CL3/2/CD parameter. The investigation was performed both numerically and experimentally starting from airfoils and winglet shape design. Given the shape of a real hang-glider wing under aerodynamic load the first phase of the work concerned the main geometric characteristics of winglet design : number of winglets, airfoils, planform shape, twist. A 3D wing model was built and using the indications obtained from the design, different sets of winglets were built. The wing model was built to enable winglets to be applied to the wing tip without changing the wing span and aspect ratio. The te...
This article is focused on numerical investigations aimed to analyze the advantages induced on high ...
Aeronautic and aerospace engineering is recently moving in the direction of developing morphing wing...
Although theoretical tools for the design of winglets for low-speed aircraft were initially of limit...
The main aim of the present paper is to investigate the influence of multiple winglets on hang-glide...
The main aim of the present paper is to investigate the influence of multiple winglets on hang-glide...
The main aim of the present paper is to investigate the influence of multiple winglets on hang-glide...
The main aim of the present paper is to investigate the influence of multiple winglets on hang-glide...
The main goal of the proposed paper is the numerical and experimental investigation of multiple wing...
Description: Induced drag is more and more a parameter that is examined for efficiency gains in airc...
Although theoretical tools for the design of winglets for high-performance sailplanes were initially...
abstract: Winglets and wingtip structures have been prominent in commercial aircraft design in the p...
This diploma thesis describes the design of winglets for LS-3 glider. The method for determination o...
This paper is focused on numerical investigations that analyze the advantages obtained from high-asp...
This article deals with aerodynamic and structural calculations of several wing designs to compare t...
In this article, the growth of aerodynamic efficiency and the growth of the wing structural stress i...
This article is focused on numerical investigations aimed to analyze the advantages induced on high ...
Aeronautic and aerospace engineering is recently moving in the direction of developing morphing wing...
Although theoretical tools for the design of winglets for low-speed aircraft were initially of limit...
The main aim of the present paper is to investigate the influence of multiple winglets on hang-glide...
The main aim of the present paper is to investigate the influence of multiple winglets on hang-glide...
The main aim of the present paper is to investigate the influence of multiple winglets on hang-glide...
The main aim of the present paper is to investigate the influence of multiple winglets on hang-glide...
The main goal of the proposed paper is the numerical and experimental investigation of multiple wing...
Description: Induced drag is more and more a parameter that is examined for efficiency gains in airc...
Although theoretical tools for the design of winglets for high-performance sailplanes were initially...
abstract: Winglets and wingtip structures have been prominent in commercial aircraft design in the p...
This diploma thesis describes the design of winglets for LS-3 glider. The method for determination o...
This paper is focused on numerical investigations that analyze the advantages obtained from high-asp...
This article deals with aerodynamic and structural calculations of several wing designs to compare t...
In this article, the growth of aerodynamic efficiency and the growth of the wing structural stress i...
This article is focused on numerical investigations aimed to analyze the advantages induced on high ...
Aeronautic and aerospace engineering is recently moving in the direction of developing morphing wing...
Although theoretical tools for the design of winglets for low-speed aircraft were initially of limit...