VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-propellant stages and a liquid propellant upper module. It is approximately 30 metres high, has a maximum diameter of 3 metres, and weights a total of 137 tons at lift-off. The acoustic loads applied to the launch vehicle upon the lift-off and the transonic flight, are broad band and random loads which may be dangerous for the payload and the equipment. A fast and cheap prediction may be obtained by numerical procedures rather than performing measurements on real prototypes. The classical numerical techniques (finite elements (FEM), boundary elements (BEM)) allow to predict the response of the mechanical systems at low frequency ranges, typical...
A method for estimating the structural vibration properties of complex systems in high frequency env...
This work describes the main aspects of the extended experimental campaign aimed atthe characterizat...
The approximate vibrational and acoustical responses of structural-acoustic systems can be modeled b...
In the framework of the European Space Agency funded program VECEP, aimed at further increasing the...
VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-pr...
The verification of a space launcher at the design level is a complex issue because of (i) the lack ...
ABSTRACT: Finite element method (FEM) and boundary element method (BEM) are methods usually applied ...
The verification of a space launcher at the design level is a complex issue because of (i) the lack ...
Future aircraft concepts utilizing innovative lightweight structures and novel propulsion concepts a...
During ballistic flight, a re-entry vehicle is subjected to high-level structural vibrations due to ...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
International audienceThe launch vehicles are subjected at lift-off and during flight ascent to a se...
At present, several numerical prediction techniques are available for the steady-state dynamic analy...
Abstract During flight missions launch vehicles are subjected to a severe dynamic pressure loading ...
Currently, vibroacoustic problems can be solved using a wide range of numerical techniques. In the l...
A method for estimating the structural vibration properties of complex systems in high frequency env...
This work describes the main aspects of the extended experimental campaign aimed atthe characterizat...
The approximate vibrational and acoustical responses of structural-acoustic systems can be modeled b...
In the framework of the European Space Agency funded program VECEP, aimed at further increasing the...
VEGA, the future European small launch vehicle, is a single-body launcher composed of three solid-pr...
The verification of a space launcher at the design level is a complex issue because of (i) the lack ...
ABSTRACT: Finite element method (FEM) and boundary element method (BEM) are methods usually applied ...
The verification of a space launcher at the design level is a complex issue because of (i) the lack ...
Future aircraft concepts utilizing innovative lightweight structures and novel propulsion concepts a...
During ballistic flight, a re-entry vehicle is subjected to high-level structural vibrations due to ...
Aerospace payloads, such as satellites, are subjected to vibroacoustic excitation during launch. San...
International audienceThe launch vehicles are subjected at lift-off and during flight ascent to a se...
At present, several numerical prediction techniques are available for the steady-state dynamic analy...
Abstract During flight missions launch vehicles are subjected to a severe dynamic pressure loading ...
Currently, vibroacoustic problems can be solved using a wide range of numerical techniques. In the l...
A method for estimating the structural vibration properties of complex systems in high frequency env...
This work describes the main aspects of the extended experimental campaign aimed atthe characterizat...
The approximate vibrational and acoustical responses of structural-acoustic systems can be modeled b...