The dynamic response analysis to simulate the complicated working condition can ensure the high reliability of space products' design. In this paper, we focus on the solar array of a satellite, and gain equivalent mechanical parameters of its internal honeycomb panel's construction. We build an accurate finite element model, and perform modal analysis and frequency response analysis as well. By contrast, the simulation data matches experimental results well, which provides important reference for subsequent structure optimization and improvement
The modal analysis of a satellite sailboard finite element model is carried out to accurately invest...
The modal analysis of a satellite sailboard finite element model is carried out to accurately invest...
sciences mission, analysis of data from the rst 370 days after launch was used to investigate in- ...
The dynamic response analysis to simulate the complicated working condition can ensure the high reli...
This paper describes the structural analysis carried out on the main stiffened and honeycomb panels ...
Due to the difficulty of direct finite-element modeling for honeycomb sandwich panels, it is more co...
Due to the difficulty of direct finite-element modeling for honeycomb sandwich panels, it is more co...
Due to the difficulty of direct finite-element modeling for honeycomb sandwich panels, it is more co...
Abstract Aerospace products need to simulate the complicated working conditions through dynamic simu...
Abstract Aerospace products need to simulate the complicated working conditions through dynamic simu...
Aerospace products need to simulate the complicated working conditions through dynamic simulation an...
The purpose of the present thesis is to furnish diverse studies on the dynamic response of satellite...
Understanding the dynamic characteristics of solar arrays is important for satellite structural desi...
In order to be cost-effective, space structures must be extremely light-weight, and subsequently, ve...
The modal analysis of a satellite sailboard finite element model is carried out to accurately invest...
The modal analysis of a satellite sailboard finite element model is carried out to accurately invest...
The modal analysis of a satellite sailboard finite element model is carried out to accurately invest...
sciences mission, analysis of data from the rst 370 days after launch was used to investigate in- ...
The dynamic response analysis to simulate the complicated working condition can ensure the high reli...
This paper describes the structural analysis carried out on the main stiffened and honeycomb panels ...
Due to the difficulty of direct finite-element modeling for honeycomb sandwich panels, it is more co...
Due to the difficulty of direct finite-element modeling for honeycomb sandwich panels, it is more co...
Due to the difficulty of direct finite-element modeling for honeycomb sandwich panels, it is more co...
Abstract Aerospace products need to simulate the complicated working conditions through dynamic simu...
Abstract Aerospace products need to simulate the complicated working conditions through dynamic simu...
Aerospace products need to simulate the complicated working conditions through dynamic simulation an...
The purpose of the present thesis is to furnish diverse studies on the dynamic response of satellite...
Understanding the dynamic characteristics of solar arrays is important for satellite structural desi...
In order to be cost-effective, space structures must be extremely light-weight, and subsequently, ve...
The modal analysis of a satellite sailboard finite element model is carried out to accurately invest...
The modal analysis of a satellite sailboard finite element model is carried out to accurately invest...
The modal analysis of a satellite sailboard finite element model is carried out to accurately invest...
sciences mission, analysis of data from the rst 370 days after launch was used to investigate in- ...