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Juan A. Sillero

Researcher at Technical University of Madrid

Publications -  23
Citations -  1086

Juan A. Sillero is an academic researcher from Technical University of Madrid. The author has contributed to research in topics: Boundary layer & Reynolds number. The author has an hindex of 9, co-authored 23 publications receiving 906 citations. Previous affiliations of Juan A. Sillero include Yale University.

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One-point statistics for turbulent wall-bounded flows at Reynolds numbers up to δ+ ≈ 2000

TL;DR: One-point statistics are presented for new direct simulations of the zero-pressure-gradient turbulent boundary layer in the range Reθ = 2780-6680, matching channels and pipes at δ+ ≈ 1000-2000 as discussed by the authors.
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Two-point statistics for turbulent boundary layers and channels at Reynolds numbers up to δ + ≈ 2000

TL;DR: In this article, three-dimensional spatial correlations are investigated in very long domains to educe the average structure of the velocity and pressure fluctuations in the zero-pressure-gradient turbulent boundary layer in the range Re θ = 2780-6680.
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IMS-MS studies based on coupling a differential mobility analyzer (DMA) to commercial API-MS systems

TL;DR: In this article, a two-dimensional differential mobility analyzer (DMA)-MS spectra of multiply charged clusters formed in electrosprays of concentrated solutions of tetrahexylammonium bromide (A+Br−) were obtained.
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A code for direct numerical simulation of turbulent boundary layers at high Reynolds numbers in BG/P supercomputers

TL;DR: In this article, a new high-resolution code for the direct numerical simulation of a zero pressure gradient turbulent boundary layers over a flat plate has been developed, which is used to simulate a wide range of Reynolds numbers from Reθ = 300 to 6800.
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Direct numerical simulation of a self-similar adverse pressure gradient turbulent boundary layer

TL;DR: The statistical properties of a self-similar adverse pressure gradient (APG) turbulent boundary layer (TBL) are presented in this paper, which is generated via the direct numerical simulation of a TBL on a flat surface with a farfield boundary condition designed to apply the desired pressure gradient.