Virtual testing for the prediction of damping in joints

被引:19
作者
Caignot, A. [1 ]
Ladeveze, P. [1 ]
Neron, D. [1 ]
Durand, J. -F. [2 ]
机构
[1] ENS Cachan CNRS UPMC PRES UniverSud Paris, LMT Cachan, Cachan, France
[2] Launchers & ATV Mech Engn Struct Dynam, ASTRIUM ST, Les Mureaux, France
关键词
Damping; Predictive process; Spacecraft; Parallel programming; Performance testing; BOLTED JOINTS; FRICTION; MODELS;
D O I
10.1108/02644401011050912
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Purpose - The purpose of this paper is to propose a virtual testing strategy in order to predict damping due to the joints which are present in the ARIANE 5 launcher Design/methodology/approach - Since engineering finite element codes do not give satisfactory results, either because they are too slow or because they cannot calculate dissipation accurately, a new computational tool is introduced based on the LArge Time INcrement (LATIN) method in its multiscale version. Findings - The capabilities of the new strategy are illustrated on one of the joints of ARIANE 5. The damping predicted virtually is compared to experimental results, and the approach appears promising. Originality/value - The tool which has been developed gives access to calculations which were previously unaffordable with standard computational codes, which may improve the design process of launchers. The code is transferred into ASTRIUM-ST, where it is being used to build a database of dissipations in the joints of the ARIANE 5 launcher.
引用
收藏
页码:621 / 644
页数:24
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