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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 65
FINITE ELEMENTS: TECHNIQUES AND DEVELOPMENTS Edited by: B.H.V. Topping
Paper X.6
Automatic Time Stepping Algorithms for Implicit Numerical Simulations of Non-Linear Dynamics L. Noels, L. Stainier, J.P. Ponthot and J. Bonini
Laboratoire de Techniques Aéronautiques et Spatiales, Université de Liège, Liège, Belgium L. Noels, L. Stainier, J.P. Ponthot, J. Bonini, "Automatic Time Stepping Algorithms for Implicit Numerical Simulations of Non-Linear Dynamics", in B.H.V. Topping, (Editor), "Finite Elements: Techniques and Developments", Civil-Comp Press, Edinburgh, UK, pp 263-272, 2000. doi:10.4203/ccp.65.10.6
Abstract
Variable step strategies are specially well suited to deal with
problems characterized by high non-linearity and
contact/impact. Both phenomena are typical of dynamic
simulations of the interactions between a turbine blade and its
casing, the most dramatic example being blade loss. Constant
step size strategies do not give satisfactory answer for this
kind of problems, since it is very difficult, if not impossible,
for the user to find an appropriate time step that does not lead
to divergence nor generate extremely costly computations.
An automatic time stepping algorithm is proposed, which
takes into account the recent history of accelerations in the
bodies under consideration. More precisely, the adaptation
algorithm is based on estimators of the integration error of
the differential dynamic balance equations. This allows for
adaptation of the time step to capture correctly the transient
phenomena, with characteristic times which can range from
relatively long (in regime) to very short (blade loss), thus
ensuring precision while keeping the computation cost to a
minimum. Additionally, the proposed algorithm
automatically takes decisions regarding the necessity of
updating the tangent matrix or stopping the iterations, further
reducing the computational cost. As an illustration of the
capabilities of this algorithm, several numerical simulations
of both academic and industrial (the contact/impact between
a turbine blade and the casing) problems will be presented.
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