Simulation of the shock wave boundary layer interaction in flat channel with jet injection

DOI10.1002/ZAMM.202200375OpenAlexW4316276750MaRDI QIDQ6121596

Unnamed Author, A. Zh. Naimanova, Unnamed Author, Unnamed Author

Publication date: 26 March 2024

Published in: ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/zamm.202200375

zbMATH Keywords

supersonic flowFavre-averaged Navier-Stokes equationsfourth-order weighted essentially non-oscillatory schemek-omega turbulence model

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite volume methods applied to problems in fluid mechanics (76M12) Turbulent boundary layers (76F40) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20) Compressible Navier-Stokes equations (76N06)

Cites Work

• Vortical structures behind a transverse jet in a supersonic flow at high jet to crossflow pressure ratios
• Numerical study of spatial supersonic flow of a perfect gas with transverse injection of jets
• Boundary conditions for direct simulations of compressible viscous flows
• Weighted essentially non-oscillatory schemes

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