Instytut Podstawowych Problemów Techniki
Polskiej Akademii Nauk

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Ludovic Blanc

French-German Research Institute of Saint-Louis (FR)

Ostatnie publikacje
1.  Stańczak M., Frąś T., Blanc L., Pawłowski P., Rusinek A., Blast-induced compression of a thin-walled aluminum honeycomb structure—experiment and modeling, Metals, ISSN: 2075-4701, DOI: 10.3390/met9121350, Vol.9, No.12, pp.1350-1-24, 2019

Streszczenie:
The presented discussion concerns the behavior of a thin-walled hexagonal aluminum honeycomb structure subjected to blast loading. The shock wave affecting the structure is generated by detonation of the C4 charge in an explosive-driven shock tube (EDST). The EDST set-up is an instrumented device that makes it possible to study blast effects in more stable and repeatable conditions than those obtained in a free-air detonation. The formation of folds characteristic of a honeycomb deformation in the axial compression distributes the initial loading over a time period, which is considered as an efficient method of energy dissipation. The test configuration is modeled in the Ls-Dyna explicit code, which enables analysis of the mechanisms of energy absorption that accompanies structural deformation under a blast loading. The conclusions reached in the performed experimental and numerical investigation can be applied to the modeling and optimization of cellular structures used to mitigate blast loadings.

Słowa kluczowe:
thin-walled hexagonal aluminum honeycomb, dynamic compression, blast energy absorption, EDST, numerical simulation of blast effects

Afiliacje autorów:
Stańczak M. - French-German Research Institute of Saint-Louis (FR)
Frąś T. - French-German Research Institute of Saint-Louis (FR)
Blanc L. - French-German Research Institute of Saint-Louis (FR)
Pawłowski P. - IPPT PAN
Rusinek A. - inna afiliacja
70p.

Prace konferencyjne
1.  Stanczak M., Fras T., Blanc L., Pawlowski P., Rusinek A., Numerical and experimental study on mechanical behaviour of the AlSi10Mg aluminium structures manufactured additively and subjected to a blast wave, DYMAT 2021, 13TH INTERNATIONAL CONFERENCE ON MECHANICAL AND PHYSICAL BEHAVIOUR OF MATERIALS UNDER DYNAMIC LOADING, 2021-09-20/09-24, Madryt (ES), DOI: 10.1051/epjconf/202125002017, Vol.250, pp.02017-1-8, 2021

Streszczenie:
The paper is related to the energy absorptive properties of additively manufactured metallic cellular structures. The samples of Honeycomb, Auxetic, rhomboidal Lattice and a regular Foam are subjected to dynamic compression due to the blast tests. The cuboidal samples are manufactured by the Direct Metal Laser Sintering (DMLS) method using AlSi10Mg aluminium powder. The experimental tests are performed by means of an Explosive Driven Shock Tube (EDST). The measured results of the transmitted forces in relation to the shortening of the samples allow to analyse of the deformation processes of each selected geometry. In addition, the evaluation of the structural responses leads to the identification of the structure properties, such as the equivalent stress over equivalent strain or the energy absorption per a unit of mass. Moreover, the process of compression is modelled numerically using the explicit code LS-DYNA R9.0.1. The obtained simulations provide the complete analysis of the experimentally observed mechanisms.

Afiliacje autorów:
Stanczak M. - inna afiliacja
Fras T. - inna afiliacja
Blanc L. - French-German Research Institute of Saint-Louis (FR)
Pawlowski P. - IPPT PAN
Rusinek A. - IPPT PAN
2.  Stańczak M., Frąś T., Blanc L., Pawłowski P., Rusinek A., Numerical Modeling of Honeycomb Structure Subjected to Blast Loading, LS-DYNA2019, 12th European LS-DYNA Conference 2019, 2019-05-14/05-16, Koblenz (DE), pp.1-10, 2019

Streszczenie:
The main objective of this study is related to the modeling of an aluminum thin-walled honeycomb structure under blast loading. The blast test is performed by means of an explosively driven shock tube (EDST). A planar shock wave is generated by a small amount of an explosive charge detonated in front of the tube. The honeycomb core is compressed by a movement of the steel plate located at the end of the tube. In the experiment, the honeycomb deformation is recorded by a high-speed camera and the absorbed loading by the structure is measured by a force sensor fixed on the rear sample face. The simulation of the material behavior is carried out using the Lagrangian approach implemented in LS-DYNA, ver. R9.0.1. The shock pressure generated by the explosion is recalculated to define the force applied to the plate being in contact (*AUTOMATIC_SURFACE_TO_SURFACE with friction) with the honeycomb and causing its deformation. The honeycomb is meshed by shell elements with a default formulation ELFORM: BELYTSCHKO-TSAY. The front plate is assumed as a rigid body to induce a uniform deformation of the honeycomb structure modeled using *MAT_SIMPLIFIED_JOHNSON_COOK 098 with parameters published in, [1-2]. The simulations are performed for different number of unit cells to define the honeycomb, from a single cell to fifty-three cells, aiming to indicate a minimal cell number required to model properly the entire structure. A dependence of numerical results on the mesh size, unit cell dimensions, friction conditions and the strain rate has been verified. The comparison between values of the load absorbed by the sample crushed numerically and experimentally shows a good agreement providing an insight into mechanisms of blast wave absorption by honeycomb structures. Such an analysis may be further applicable in development of advanced cellular structures applied to dissipate blast energy.

Afiliacje autorów:
Stańczak M. - French-German Research Institute of Saint-Louis (FR)
Frąś T. - French-German Research Institute of Saint-Louis (FR)
Blanc L. - French-German Research Institute of Saint-Louis (FR)
Pawłowski P. - IPPT PAN
Rusinek A. - inna afiliacja

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