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Dive into the research topics where L. Biamino is active.

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Featured researches published by L. Biamino.


Physics of Fluids | 2014

An experimental and numerical investigation of the dependency on the initial conditions of the Richtmyer-Meshkov instability

Marc Vandenboomgaerde; Denis Souffland; Christian Mariani; L. Biamino; G. Jourdan; L. Houas

The nonlinear evolution of 2D single-mode Richtmyer-Meshkov instabilities is investigated through experiments in shock tube and numerical simulations. In our shock tube, the interface is materialized by a thin membrane attached to a stereo-lithographed grid. The purpose of this study is to compare experimental and numerical results, verify that using a higher Mach number for the incident shock wave (Misw) than in a previous study [C. Mariani, M. Vandenboomgaerde, G. Jourdan, D. Souffland, and L. Houas, “Investigation of the Richtmyer-Meshkov instability with stereolithographed interfaces,” Phys. Rev. Lett. 100, 254503 (2008)] drastically reduces the deleterious effects of the membrane remnants, explore the effect of a high initial amplitude at the interface on the growth of the perturbation, and understand the lack of roll-up structures in the nonlinear phase of the instability. Using grayscale gradient rather than gray level, a new processing of the raw pictures is developed. Numerical simulations run wi...


Physics of Fluids | 2010

Experimental and numerical study of weak shock wave transmissions through minitubes

J. Giordano; Jean-Denis Parisse; L. Biamino; J. Devesvre; Pierre Perrier

The aim of this letter is to present an original experimental technique to study weak shock wave in a minitube. Thus, we designed an apparatus that can be connected to any classical shock tube in order to characterize high speed flows induced by the shock wave transmission in minitubes. We proposed appropriated measurements based on high speed strioscopy coupled with pressure sensors. Two minitube diameters are considered: 1.020±0.010 and 0.480±0.010 mm. We realized preliminary experimental and numerical campaigns with an incident shock wave Mach number at 1.12±0.01. The generation of a microshock wave was observable in the two minitubes. For the smallest minitube, we found an attenuation of the strength of the shock wave with a decrease of 1.8% of the Mach number.


International Symposium on Shock Waves | 2015

Experimental and Numerical Investigation of the Propagation of a Planar Shock Wave into a Cloud of Droplets

A. Chauvin; G. Jourdan; L. Biamino; E. Daniel; L. Houas; R. Tosello; D. Leriche

Since several decades, the interest to study the interaction between a shock wave and a two phase medium grows. First, the influence on the propagation of a shock wave by a dusty gas then by a medium composed by solid particles were investigated


International Symposium on Shock Waves | 2015

Generation of Cylindrical Converging Shock Waves in a Conventional Shock Tube

L. Biamino; G. Jourdan; Christian Mariani; L. Houas; M. Vandenboomgaerde; D. Souffland

For ever two decades, the IUSTI laboratory has been known for its investigations [1] dealing with the Richtmyer-Meshkov instability (RMI). Experiments concerning the RMI have been performed in conventional shock tubes [2, 3, 4, 5]. All these experiments use a planar shock wave to generate the instability as perfectly as possible. However, the RMI also occurs in the spherical case where the convergence effects must be taken into account. As far as we know, no conventional (straight section) shock tube facility has been used to experimentally study the RMI in a spherical geometry.


Archive | 2017

Richtmyer-Meshkov Instability in a Cylindrical Geometry Using a Conventional Shock Tube

L. Biamino; G. Jourdan; Christian Mariani; L. Houas; Marc Vandenboomgaerde; Denis Souffland

During the past 20 years, there was considerable amount of analytical, computational, and experimental works dealing with the planar version of the problem of the Richtmyer-Meshkov instability (RMI). However, this problem is often spherical, and so far there have been only few experimental studies in such configuration, except the cases of both shock-accelerated cylinders [1] and spheres [2] which can be categorized under this label. In convergent geometry, the RMI differs from the planar case due to both the geometrical effects on the instability and a different mono-dimensional (1D) motion of the interface itself. Thus, to better understand the dynamics of this instability in convergent geometry and validate models in such configuration, new experimental data are needed. Holder et al. [3] reported laboratory experiments with a convergent shock tube, using a detonable gas mixture to produce a cylindrically convergent shock. Recently, Zhai et al. [4], Apazidis et al. [5], and Biamino et al. [6] have experimentally proven the possibility of generating a converging cylindrical shock wave using a conventional shock tube. Zhai et al. proposed to design a shock tube having a curved wall test section. This specific wall converts a planar shock wave into a cylindrical one. Apazidis et al. have developed a device where the shock wave propagates inside an annular chamber and focuses after its reflection on the end-wall. Biamino et al. have used and implemented the gas lens theory revisited by Vandenboomgaerde and Aymard [7]. This theory was originally proposed by Dimotakis and Samtaney [8]. This work was the first experimental demonstration of the gas lens technique applied to the T80 conventional shock tube of IUSTI. It was shown that a planar incident shock wave propagating in air (Mis = 1.15) which refracts through a specific elliptical air/SF6 interface generates a cylindrical transmitted shock wave in a two-dimensional wedge geometry with a 30° half apex angle. We were able to diagnose the morphing and the focusing of the shock wave. This study constituted the first step toward canonical experiments on the converging RMI in shock tube environment, for which a second interface had to be implemented. Thus, a new two-dimensional wedge test section (15° half apex angle) was designed to accommodate two interfaces: a first air/SF6 interface of elliptical shape to convert the incident planar shock wave into a cylindrical converging one and a second sinusoidal SF6/air interface to study the converging RMI (see Fig. 1). In the present work, the details of this new experimental apparatus were implemented on the T80 shock tube, and the first results are reported. In particular, the evolution process of interfacial structures induced by RMI is shown.


Archive | 2017

Blast Wave Impact on a Parallelepiped Headed with a Semicylindrical Model Drilled with a Rectangular Cavity

R. Tosello; L. Biamino; D. Leriche; Christian Mariani; G. Jourdan; J.-C. Loraud; L. Houas

As part of a research program for the protection of people and buildings after an explosion, a series of experiments is carried out. After an explosion in free air, the created blast wave can penetrate into buildings, boats, or underground shelters.


Archive | 2012

Long Time Observation of the Richtmyer-Meshkov Instability

Christian Mariani; L. Biamino; G. Jourdan; L. Houas; M. Vandenboomgaerde; D. Souffland

Richtmyer-Meshkov (RM) instability occurs when a interface separating two fluids of different density is impulsively accelerated in the direction of its normal. It is one of the most fundamental fluid instabilities and is of importance to the fields of astrophysics and inertial confinement fusion. RM instability experiments are normally carried out in shock tubes, where the generation of a sharp, well-controlled interface between gases is difficult, so there is a dispersion in terms of experimental results. The experiments presented here were conducted in a horizontal shock tube where the materialization of the initial interface was achieved by a thin nitrocellulosic membrane (0.5 μm thick) deposited on a stereolithographed grid support, computer-aided designed and constructed with chosen shape and dimensions. As diagnostic, we used laser sheet flow visualization to yield time-motion image sequences of the linear and the non-linear developments of the instability. In previous investigation [1], we have already shown that residual pieces from the membrane constituting the initial interface tend to delay the interpenetration in the light-to-heavy gas configuration and specifically during the linear stage of the interface evolution. In order to reduce these effects in the present experiments, we have increased the strength of the shock wave (Mach~1.5). We have also extended the test section from 0.46 m to 1.5 m which allows the instability to grow further and thus to observe the whole nonlinear phase until the transition to turbulence. The present paper summarizes the results obtained during this study undertaken for air/SF6 and air/He gas combinations (positive and negative Atwood numbers, respectively) in 2D and 3D geometries.


Experiments in Fluids | 2015

On the possibility of studying the converging Richtmyer–Meshkov instability in a conventional shock tube

L. Biamino; G. Jourdan; Christian Mariani; L. Houas; M. Vandenboomgaerde; D. Souffland


Journal of Fluids Engineering-transactions of The Asme | 2014

Planar Shock Focusing Through Perfect Gas Lens: First Experimental Demonstration

L. Biamino; Christian Mariani; G. Jourdan; L. Houas; Marc Vandenboomgaerde; Denis Souffland


Shock Waves | 2012

The effects that changes in the diaphragm aperture have on the resulting shock tube flow

L. Houas; L. Biamino; Christian Mariani; O. Igra; G. Jourdan; A. Massol

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G. Jourdan

Aix-Marseille University

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L. Houas

Aix-Marseille University

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O. Igra

Ben-Gurion University of the Negev

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E. Daniel

Aix-Marseille University

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A. Chauvin

Aix-Marseille University

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A. Marty

Aix-Marseille University

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A. Massol

Airbus Operations S.A.S.

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J. Devesvre

Aix-Marseille University

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