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Sergey A. Karabasov

Researcher at Queen Mary University of London

Publications -  163
Citations -  1820

Sergey A. Karabasov is an academic researcher from Queen Mary University of London. The author has contributed to research in topics: Jet noise & Jet (fluid). The author has an hindex of 19, co-authored 138 publications receiving 1495 citations. Previous affiliations of Sergey A. Karabasov include University of Cambridge & Russian Academy of Sciences.

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Jet Noise: Acoustic Analogy informed by Large Eddy Simulation

TL;DR: In this article, a hybrid approach to the development of a hybrid prediction methodology for jet noise is described, where a Gaussian function model for the two-point cross correlation of the fourth-order velocity fluctuations in the acoustic source is presented.
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Compact Accurately Boundary-Adjusting high-REsolution Technique for fluid dynamics

TL;DR: A novel high-resolution numerical method is presented for one-dimensional hyperbolic problems based on the extension of the original Upwind Leapfrog scheme to quasi-linear conservation laws, which is second-order accurate on non-uniform grids in space and time.
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CABARET in the ocean gyres

TL;DR: In this article, a new high-resolution Eulerian numerical method is proposed for modeling quasigeostrophic ocean dynamics in eddying regimes, based on a second-order non-dissipative and low-dispersive conservative advection scheme called CABARET.
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New Efficient High-Resolution Method for Nonlinear Problems in Aeroacoustics

TL;DR: In this article, a new efficient numerical method for aeroacoustic applications is proposed, which combines traditional merits of finite volume and finite difference approaches such as shock capturing and linear Fourier accuracy on coarse grids.
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CABARET Method on Unstructured Hexahedral Grids for Jet Noise Computation

TL;DR: In this paper, a new scalable high-resolution CABARET MILES method coupled with a porous Ffowcs Williams-Hawking formulation for far-field noise modelling is applied for the computation of flow and noise from a high-speed turbulent jet, which corresponds to a converging axi-symmetric nozzle and static isothermal conditions of the Jet Exhaust Aerodynamics and Noise experiment.