This article will address the modeling and control of surface embedded shape memory alloys (SMAs) for the camber modification of a hybrid morphing airfoil. An analytical model will be derived. The results of this models will be discussed and compared to the experiments. The advantages of this modeling approach will be highlighted and alternatives will be briefly revisited. This discussion will figure into the utility of these models in the sizing of a full scale prototype of a SMA actuated active trailing edge of an airfoil. Throughout this article the prototype specifications are detailed and the design choices will be discussed. Performance improvements stemming from the inherent nature of the SMAs will be analyzed. It will be shown in th...
Aircraft morphing architectures are currently worldwide investigated to enhance performance while re...
Benefits in terms of aerodynamic efficiency, aeroelastic behaviour, stability and manoeuvrability pe...
The development of structures able to autonomously change their characteristics in response to an ex...
This article will address the modeling and control of surface embedded shape memory alloys (SMAs) fo...
The adaptive structures’ concept is of great interest for researchers involved in the aeronautical f...
The adaptive structures concept is of great interest in the aeronautical field because of the severa...
The adaptive structures concept is of great interest in the aerospace field because of the several b...
This article is focused on numerical and experimental investigations of smart structure concepts, de...
AbstractAn experimental morphing laminar wing was developed to prove the feasibility of aircraft fue...
Shape memory alloy (SMA) is lightweight, produces high force and large deflection which makes it a s...
In the work at hand, the development of a morphing flap, actuated through shape memory alloy load be...
ABSTRACT: Multiple flight regimes during typical aircraft missions mean that a single unique optimiz...
Based on numerical and experimental analyses, this article proposes an application of the smart stru...
Aircraft morphing architectures are currently worldwide investigated to enhance performance while re...
Benefits in terms of aerodynamic efficiency, aeroelastic behaviour, stability and manoeuvrability pe...
The development of structures able to autonomously change their characteristics in response to an ex...
This article will address the modeling and control of surface embedded shape memory alloys (SMAs) fo...
The adaptive structures’ concept is of great interest for researchers involved in the aeronautical f...
The adaptive structures concept is of great interest in the aeronautical field because of the severa...
The adaptive structures concept is of great interest in the aerospace field because of the several b...
This article is focused on numerical and experimental investigations of smart structure concepts, de...
AbstractAn experimental morphing laminar wing was developed to prove the feasibility of aircraft fue...
Shape memory alloy (SMA) is lightweight, produces high force and large deflection which makes it a s...
In the work at hand, the development of a morphing flap, actuated through shape memory alloy load be...
ABSTRACT: Multiple flight regimes during typical aircraft missions mean that a single unique optimiz...
Based on numerical and experimental analyses, this article proposes an application of the smart stru...
Aircraft morphing architectures are currently worldwide investigated to enhance performance while re...
Benefits in terms of aerodynamic efficiency, aeroelastic behaviour, stability and manoeuvrability pe...
The development of structures able to autonomously change their characteristics in response to an ex...