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Numerical Study of Crossflow Jet Generated Instabilities in a High-Speed Boundary Layer

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IUTAM Laminar-Turbulent Transition

Part of the book series: IUTAM Bookseries ((IUTAMBOOK,volume 38))

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Abstract

Numerical simulations of 3-D disturbances induced by an underexpanded jet in supersonic crossflow (JISC) in the Mach 5.4 flat-plate boundary layer (BL) are carried out. The Navier–Stokes equations for compressible perfect gas are integrated using the in-house solver implementing an implicit finite-volume shock-capturing scheme with the second-order approximation in space and time. The numerical solutions indicate that the wall normal injection through a circular hole forms an underexpanded jet of barrel shape, which induces a system of vortices propagating downstream. These vortices are destabilized at a short distance that leads to rapid nonlinear breakdown and formation of a turbulent wedge. The vortex structure, its instability and breakdown to turbulence resemble those induced by an isolated roughness element. It is shown that the normal wall injection effectively trips the BL flow. This encourages further numerical studies of active tripping of high-speed BL flows using rows of JISC.

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Acknowledgements

This work was supported by the Russian Foundation for Basic Research (project 18-08-01295 – calculations) and Russian Science Foundation (project 19-19-00470 – development of the model for flow in a channel) and has been carried out using computing resources of the federal collective usage center Complex for Simulation and Data Processing for Mega-science Facilities at NRC “Kurchatov Institute”, http://ckp.nrcki.ru/.

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Authors and Affiliations

  1. Central Aerohydrodynamic Institute, 1 Zhukovsky Street, Zhukovsky, Russia

    Andrey V. Novikov

  2. Moscow Institute of Physics and Technology (National Research University), 9 Institutskiy per., Dolgoprudny, Russia

    Andrey V. Novikov & Alexander V. Fedorov

Authors
  1. Andrey V. Novikov
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  2. Alexander V. Fedorov
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Correspondence to Andrey V. Novikov .

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Editors and Affiliations

  1. Imperial College London, London, UK

    Spencer Sherwin

  2. Imperial College London, London, UK

    Peter Schmid

  3. Imperial College London, London, UK

    Xuesong Wu

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Novikov, A.V., Fedorov, A.V. (2022). Numerical Study of Crossflow Jet Generated Instabilities in a High-Speed Boundary Layer. In: Sherwin, S., Schmid, P., Wu, X. (eds) IUTAM Laminar-Turbulent Transition. IUTAM Bookseries, vol 38. Springer, Cham. https://doi.org/10.1007/978-3-030-67902-6_54

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  • DOI: https://doi.org/10.1007/978-3-030-67902-6_54

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-030-67901-9

  • Online ISBN: 978-3-030-67902-6

  • eBook Packages: EngineeringEngineering (R0)

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