ABSTRACT: Finite element method (FEM) and boundary element method (BEM) are methods usually applied on low-frequency coupled fluid-structure analysis. On the other hand, statistical energy analysis (SEA) is a technique applied on small wavelength bandwidth predictions. However, in the mid-frequency, where deterministic calculations are costly and confidence intervals of SEA are not satisfied, hybrid FEM/SEA models can be used. This work presents a coupled vibro-acoustic analysis methodology of the Brazilian Satellite Launcher Vehicle payload fairing. FEM/FEM model accounts for the low-frequency internal responses. The high-frequency responses are computed by a SEA coupled elasto-acoustic model, and a hybrid FEM/SEA model calculates the payl...
During ballistic flight, a re-entry vehicle is subjected to high-level structural vibrations due to ...
The PhD fellow will study the hybrid evaluation of the broad frequency acoustic behaviour of lightwe...
Future aircraft concepts utilizing innovative lightweight structures and novel propulsion concepts a...
ABSTRACT: Finite element method (FEM) and boundary element method (BEM) are methods usually applied ...
Currently, vibroacoustic problems can be solved using a wide range of numerical techniques. In the l...
The acoustic environment generated during launch is the most demanding structural load case for larg...
Abstract During flight missions launch vehicles are subjected to a severe dynamic pressure loading ...
At present, several numerical prediction techniques are available for the steady-state dynamic analy...
VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-pr...
In the framework of the European Space Agency funded program VECEP, aimed at further increasing the...
Based on the concept of hybrid Finite Element (FE) analysis and Statistical Energy Analysis (SEA), a...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
This work focuses on the analysis of a structural element of MetOP-A satellite. Given the special in...
New developments in the hybrid Finite Element Analysis (hybrid FEA) are presented in this Thesis. Th...
Most of the currently available numerical prediction techniques for the analysis of steady-state dyn...
During ballistic flight, a re-entry vehicle is subjected to high-level structural vibrations due to ...
The PhD fellow will study the hybrid evaluation of the broad frequency acoustic behaviour of lightwe...
Future aircraft concepts utilizing innovative lightweight structures and novel propulsion concepts a...
ABSTRACT: Finite element method (FEM) and boundary element method (BEM) are methods usually applied ...
Currently, vibroacoustic problems can be solved using a wide range of numerical techniques. In the l...
The acoustic environment generated during launch is the most demanding structural load case for larg...
Abstract During flight missions launch vehicles are subjected to a severe dynamic pressure loading ...
At present, several numerical prediction techniques are available for the steady-state dynamic analy...
VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-pr...
In the framework of the European Space Agency funded program VECEP, aimed at further increasing the...
Based on the concept of hybrid Finite Element (FE) analysis and Statistical Energy Analysis (SEA), a...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
This work focuses on the analysis of a structural element of MetOP-A satellite. Given the special in...
New developments in the hybrid Finite Element Analysis (hybrid FEA) are presented in this Thesis. Th...
Most of the currently available numerical prediction techniques for the analysis of steady-state dyn...
During ballistic flight, a re-entry vehicle is subjected to high-level structural vibrations due to ...
The PhD fellow will study the hybrid evaluation of the broad frequency acoustic behaviour of lightwe...
Future aircraft concepts utilizing innovative lightweight structures and novel propulsion concepts a...