The study presented in this paper concerns the development of an algorithm, based on finite element analysis, for the dynamic simulation of a tethered lighter-than-air balloon when subjected to operational conditions. The main features of the algorithm are described, highlighting the advantages of this approach when performing dynamic analysis. The input parameters considered in the method are derived from experimental and simulated data, which are elaborated to obtain the static and dynamic atmospheric properties in terms of mean windspeed profile, discrete gusts, and continuous turbulence. In particular, the algorithm is employed to perform a thorough analysis of a specific high-altitude tethered platform operating in a realistic design s...
The Airborne Wind Energy (AWE) is a growing field of research that intends to develop solutions for ...
The kite is modelled with the non-linear finite element method to stay close to its physical propert...
The objective of this research is the simulation of aero-elastic behaviour of Makani’s large airborn...
The study presented in this paper concerns the development of an algorithm, based on finite element ...
This paper illustrates a procedure to calculate the response of a tethered spherical aerostat to gus...
This paper illustrates a procedure to calculate the response of a tethered spherical aerostat to gus...
This research involves the development of a full 3-dimensional nonlinear model of a tethered aerosta...
This paper describes a model that has been developed to study the stability characteristics of aeros...
Mathematical tools were developed previously to analyze the dynamic behavior of tethered balloon sys...
A balloon tethered at an altitude of 20 km could deliver a particulate cloud leading to global cooli...
This paper presents an extension of the simulation code ASWING to aeroelastic analysis of an airborn...
The dynamics of open balloons in an atmosphere may be studied with a body-fluid coupled model. A num...
This paper presents an extension of the simulation code ASWING to aeroelastic analysis of an airborn...
This thesis investigates the dynamic modelling of a kite power system. The goal was to create a mode...
In this paper, we present a numerical study of a stratospheric balloon system tethered to a passive ...
The Airborne Wind Energy (AWE) is a growing field of research that intends to develop solutions for ...
The kite is modelled with the non-linear finite element method to stay close to its physical propert...
The objective of this research is the simulation of aero-elastic behaviour of Makani’s large airborn...
The study presented in this paper concerns the development of an algorithm, based on finite element ...
This paper illustrates a procedure to calculate the response of a tethered spherical aerostat to gus...
This paper illustrates a procedure to calculate the response of a tethered spherical aerostat to gus...
This research involves the development of a full 3-dimensional nonlinear model of a tethered aerosta...
This paper describes a model that has been developed to study the stability characteristics of aeros...
Mathematical tools were developed previously to analyze the dynamic behavior of tethered balloon sys...
A balloon tethered at an altitude of 20 km could deliver a particulate cloud leading to global cooli...
This paper presents an extension of the simulation code ASWING to aeroelastic analysis of an airborn...
The dynamics of open balloons in an atmosphere may be studied with a body-fluid coupled model. A num...
This paper presents an extension of the simulation code ASWING to aeroelastic analysis of an airborn...
This thesis investigates the dynamic modelling of a kite power system. The goal was to create a mode...
In this paper, we present a numerical study of a stratospheric balloon system tethered to a passive ...
The Airborne Wind Energy (AWE) is a growing field of research that intends to develop solutions for ...
The kite is modelled with the non-linear finite element method to stay close to its physical propert...
The objective of this research is the simulation of aero-elastic behaviour of Makani’s large airborn...