Prediction of Mach stem height in compressible open jets. Part 1. Overexpanded jets

DOI10.1017/JFM.2022.374OpenAlexW4281889204MaRDI QIDQ5080977

Rajesh Gopalapillai, Sushmitha Janakiram, Vinoth Paramanantham

Publication date: 1 June 2022

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2022.374

zbMATH Keywords

supersonic flowshock waveregular reflectionMach reflectionsubsonic region

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Gas dynamics (general theory) (76N15) Supersonic flows (76J20)

Cites Work

• Unnamed Item
• Shock wave reflection phenomena
• A new type of finite volume WENO schemes for hyperbolic conservation laws
• Efficient implementation of weighted ENO schemes
• An improved weighted essentially non-oscillatory scheme for hyperbolic conservation laws
• Time history of regular to Mach reflection transition in steady supersonic flow
• A study of the flow structure for Mach reflection in steady supersonic flow
• Viscous simulation of shock-reflection hysteresis in overexpanded planar nozzles
• Riemann Solvers and Numerical Methods for Fluid Dynamics
• Engineering approach to the prediction of shock patterns in bounded high-speed flows
• A parametric study of Mach reflection in steady flows
• On the Choice of Wavespeeds for the HLLC Riemann Solver
• Shock transformation and hysteresis in underexpanded confined jets
• Turbulent mixing noise from supersonic jets
• Size and shape of shock waves and slipline for Mach reflection in steady flow

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