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Johan Steelant

Researcher at European Space Research and Technology Centre

Publications -  107
Citations -  1588

Johan Steelant is an academic researcher from European Space Research and Technology Centre. The author has contributed to research in topics: Mach number & Supersonic speed. The author has an hindex of 21, co-authored 99 publications receiving 1372 citations. Previous affiliations of Johan Steelant include University of Orléans.

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Modeling of Laminar-Turbulent Transition for High Freestream Turbulence

TL;DR: In this paper, the conditionally averaged Navier-Stokes equations are used to simulate transitional skin friction or heat transfer, and a turbulence weighting factor τ is used to describe the diffusion of freestream turbulence into the boundary layer and the intermittent laminar-turbulent flow behavior during transition.
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Transitional shock-wave/boundary-layer interactions in hypersonic flow

TL;DR: In this article, the authors compared results for transitional interactions on a flat plate at Mach 6 from three different experimental facilities using the same instrumented plate insert, including a Ludwieg tube, an open-jet wind tunnel and a high-enthalpy free-piston-driven reflected shock tunnel (HEG).
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Towards a unified treatment of fully flashing sprays

TL;DR: In this article, the authors present a systematic study on flashing atomisation, which includes both standards and retrograde fluids, and propose a novel data reduction method in terms of the controlling parameters for (bubble) nucleation.
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Computational Treatment of Source Terms in Two-Equation Turbulence Models

TL;DR: Different two-equation turbulence models are investigated confirming the generality of the approach and a comparison of both methods shows that the latter is generally applicable and superior to the first, approximate method with respect to convergence speed.
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Experimental Investigations on Transpiration Cooling for Scramjet Applications Using Different Coolants

TL;DR: In this article, an approach based upon simplified analytical models is presented to analyze the experimental data of throughflow behavior and cooling efficiency and a simplified thermal model is used to analyse the effect of fluid property variations with temperature on pressure loss for different coolants.