Add to ORKGIn a wind tunnel experiment a morphing wing with span extension and camber morphing was investigated. The considered aircraft is an unmanned aerial vehicle (UAV) with a span of 4 m. During the investigations a half wing model was analysed with pressure and structural measurement. The half wing model has three different morphing mechanisms. The focus is on the morphing leading edge concept, which will be shortly described with the main objectives. First of all the morphing leading edge will be described. Afterwards the results of the wind tunnel measurement for pressure distribution, balance and deformation measurement will be presented and discussed.Aerospace Structures & Computational Mechanic
This paper presents the results obtained from the numerical simulation and experimental wind tunnel ...
This paper describes the activities performed at Politecnico di Milano within the FP7–NOVEMOR Projec...
The aim of this work is to illustrate a new wing morphing concept and to compare its performance wit...
In a wind tunnel experiment a morphing wing with span extension and camber morphing was investigated...
In a wind tunnel experiment a morphing wing with span extension and camber morphing was investigated...
The research presented in this present paper was done within the framework of the international CRIA...
A full scale morphing wing tip demonstrator with a droop-nose adaptive morphing wingtip was wind tun...
A description of a framework for a morphing leading edge will be given. The considered aircraft is ...
The common challenge of all aerospace advancements is greening the air transport. This led the rece...
Morphing technologies bare a great potential for further improvements of aircraft in terms of aerody...
The research presented in this present paper was done within the framework of the international CRIA...
The paper describes the activities performed at Politecnico di Milano in the framework of FP7-NOVEMO...
The Smart Morphing & Sensing (SMS) project was a multi-disciplinary upstream project that invest...
Morphing aircraft can change their shape radically when confronted with a variety of conflicting fli...
This article presents an experimental evaluation of a morphing leading edge demonstrator by investig...
This paper presents the results obtained from the numerical simulation and experimental wind tunnel ...
This paper describes the activities performed at Politecnico di Milano within the FP7–NOVEMOR Projec...
The aim of this work is to illustrate a new wing morphing concept and to compare its performance wit...
In a wind tunnel experiment a morphing wing with span extension and camber morphing was investigated...
In a wind tunnel experiment a morphing wing with span extension and camber morphing was investigated...
The research presented in this present paper was done within the framework of the international CRIA...
A full scale morphing wing tip demonstrator with a droop-nose adaptive morphing wingtip was wind tun...
A description of a framework for a morphing leading edge will be given. The considered aircraft is ...
The common challenge of all aerospace advancements is greening the air transport. This led the rece...
Morphing technologies bare a great potential for further improvements of aircraft in terms of aerody...
The research presented in this present paper was done within the framework of the international CRIA...
The paper describes the activities performed at Politecnico di Milano in the framework of FP7-NOVEMO...
The Smart Morphing & Sensing (SMS) project was a multi-disciplinary upstream project that invest...
Morphing aircraft can change their shape radically when confronted with a variety of conflicting fli...
This article presents an experimental evaluation of a morphing leading edge demonstrator by investig...
This paper presents the results obtained from the numerical simulation and experimental wind tunnel ...
This paper describes the activities performed at Politecnico di Milano within the FP7–NOVEMOR Projec...
The aim of this work is to illustrate a new wing morphing concept and to compare its performance wit...