2013
DOI: 10.5194/ms-4-49-2013
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CHRONO: a parallel multi-physics library for rigid-body, flexible-body, and fluid dynamics

Abstract: Abstract. The last decade witnessed a manifest shift in the microprocessor industry towards chip designs that promote parallel computing. Until recently the privilege of a select group of large research centers, Teraflop computing is becoming a commodity owing to inexpensive GPU cards and multi to many-core x86 processors. This paradigm shift towards large scale parallel computing has been leveraged in Chrono, a freely available C++ multi-physics simulation package. Chrono is made up of a collection of loosely… Show more

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Cited by 66 publications
(50 citation statements)
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“…The numerical experiments reported herein were carried out using Chrono, a library for rigid and flexible body dynamics [Mazhar et al 2013b].…”
Section: Numerical Experimentsmentioning
confidence: 99%
“…The numerical experiments reported herein were carried out using Chrono, a library for rigid and flexible body dynamics [Mazhar et al 2013b].…”
Section: Numerical Experimentsmentioning
confidence: 99%
“…The results reported in [64,65] drew on models with close to one million degrees of freedom and thus provide ample opportunities for parallel computing. For the specifics of a parallel implementation of the FSI solution, the interested reader is referred to [42].…”
Section: Mbd: the Need For Parallel Computingmentioning
confidence: 99%
“…Finally, MPI-enabled distributed computing is used to investigate the dynamics of a wheeled vehicle operating on discrete deformable terrain. These models were run in Chrono, an open source parallel simulation framework for computational dynamics [42,72].…”
Section: Software Development Aspectsmentioning
confidence: 99%
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“…Adequate representation of the soil dynamic properties [13][14][15] as well as the lander structure [16] and shock absorbing characteristics [17] are key parameters for determining the equivalent friction between the lander and the soil. Also, a proper selection of a number of parameters [18] such as the vertical and lateral landing velocities and the spacecraft inclination angle of the landing target can determine the margin of risk to crash, bounce or tip over during landing.…”
mentioning
confidence: 99%