Abstract. We present here a numerical study of the aeroelastic behavior of a pressurized flexible airship (blimp) during a flight with an angle of attack of 20◦. The airship is rep-resented by a 6:1 prolate spheroid generic geometry. The air flow is fully turbulent and is modeled by a LES model. We solve the Navier-Stokes three-dimensional compressible equations in their ALE form. The spatial discretization of these equations is achieved on unstructured tetrahedral meshes by a Finite Volumes/Finite Elements (FV/FE) mixed for-mulation. This fluid simulation is coupled to a structure solver by a staggered algorithm. We investigate a flexible pressurized hull compared to a non-pressurized one
Turbulent separated flows around an airship-like geometry (a prolate spheroid 6:1) are investigated ...
An aeroelastic modelling of an axisymmetrical airship is discussed in this paper. The main difficult...
Abstract. An aeroelastic modelling of an axisymmetrical airship is discussed in this paper. The main...
We present here a numerical study of the aeroelastic behavior of a pressurized flexible airship (bli...
In this presentation we consider a generic airship [3] which can be modelled by an ellipsoid. When t...
Stratospheric airship has great advantages, such as long-endurance, large coverage area, low-cost an...
AbstractFluid–structure interaction is an important issue for non-rigid airships with inflated envel...
Fluid-structure interaction is an important issue for non-rigid airships with inflated envelopes. In...
Effects of fluid-structure coupling on the dynamic behaviour of flexible airship can be modelled wit...
The non-rigid airship is a low-rigidity and inflatable aircraft which has obvious fluid-structure in...
Directeurs de thèse : Elie Hachem et Thomas Toulorge.We have present a full Eulerian approach to dea...
International audienceThis paper presents an efficient modelling of autonomous flexible airships. Th...
Directeurs de thèse : Elie Hachem et Thomas Toulorge.We have present a full Eulerian approach to dea...
Paper No. ESDA2006-95741Volume 3: Dynamic Systems and Controls, Symposium on Design and Analysis of ...
Paper No. ESDA2006-95741Volume 3: Dynamic Systems and Controls, Symposium on Design and Analysis of ...
Turbulent separated flows around an airship-like geometry (a prolate spheroid 6:1) are investigated ...
An aeroelastic modelling of an axisymmetrical airship is discussed in this paper. The main difficult...
Abstract. An aeroelastic modelling of an axisymmetrical airship is discussed in this paper. The main...
We present here a numerical study of the aeroelastic behavior of a pressurized flexible airship (bli...
In this presentation we consider a generic airship [3] which can be modelled by an ellipsoid. When t...
Stratospheric airship has great advantages, such as long-endurance, large coverage area, low-cost an...
AbstractFluid–structure interaction is an important issue for non-rigid airships with inflated envel...
Fluid-structure interaction is an important issue for non-rigid airships with inflated envelopes. In...
Effects of fluid-structure coupling on the dynamic behaviour of flexible airship can be modelled wit...
The non-rigid airship is a low-rigidity and inflatable aircraft which has obvious fluid-structure in...
Directeurs de thèse : Elie Hachem et Thomas Toulorge.We have present a full Eulerian approach to dea...
International audienceThis paper presents an efficient modelling of autonomous flexible airships. Th...
Directeurs de thèse : Elie Hachem et Thomas Toulorge.We have present a full Eulerian approach to dea...
Paper No. ESDA2006-95741Volume 3: Dynamic Systems and Controls, Symposium on Design and Analysis of ...
Paper No. ESDA2006-95741Volume 3: Dynamic Systems and Controls, Symposium on Design and Analysis of ...
Turbulent separated flows around an airship-like geometry (a prolate spheroid 6:1) are investigated ...
An aeroelastic modelling of an axisymmetrical airship is discussed in this paper. The main difficult...
Abstract. An aeroelastic modelling of an axisymmetrical airship is discussed in this paper. The main...