2018
DOI: 10.1007/s13272-018-0313-4
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Propeller blade debris kinematics

Abstract: The paper presents numerical models and simulations performed at ONERA in order to investigate aerodynamic effects on the trajectory of an open rotor blade fragment released or lost during an engine burst event. The models are based on Finite Elements for the structural part and on Finite Volumes for the fluid part and are implemented in the EUROPLEXUS explicit code. Fluid-Structure Interaction (FSI) is taken into account by an embedded (or immersed) technique and precision is enhanced by refining the fluid gr… Show more

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Cited by 4 publications
(2 citation statements)
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“…Recent advancements [9,12,13,14,15] in EPX allow for automatic adaptive mesh refinement (AMR) near the fluid-structure interface (FSI-driven adaptation of fluid mesh), which improves the accuracy of the embedded approach. As shown in Fig.…”
Section: Computational Methodology To Study Fsi Effectsmentioning
confidence: 99%
“…Recent advancements [9,12,13,14,15] in EPX allow for automatic adaptive mesh refinement (AMR) near the fluid-structure interface (FSI-driven adaptation of fluid mesh), which improves the accuracy of the embedded approach. As shown in Fig.…”
Section: Computational Methodology To Study Fsi Effectsmentioning
confidence: 99%
“…Each blade component mesh was deformed by means of a spring-based smoothing method, therefore adopting an arbitrary Lagrangian-Eulerian (ALE) formulation. Compared to other methods present in the literature [43], the adopted methodology can consistently preserve an appropriate y + value of the stretched cells in the region adjacent to each wall. This ensured a well-resolved near-wall flow at a reasonable computational cost.…”
Section: Fsi Couplingmentioning
confidence: 99%