Streamwise vortex breakdown due to the interaction with crossed shock waves
From MaRDI portal
Publication:6080311
DOI10.1017/jfm.2023.785OpenAlexW4387875962MaRDI QIDQ6080311
Publication date: 30 October 2023
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/jfm.2023.785
Cites Work
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
- The compressible mixing layer: an LES study
- Shock wave reflection phenomena
- Efficient implementation of weighted ENO schemes
- Numerical modeling of vortex/shock wave interaction and its transformation by localized energy deposition
- Numerical investigation of oblique shock wave/vortex interaction
- A high-order weighted compact nonlinear scheme for compressible Flows
- A family of high-order targeted ENO schemes for compressible-fluid simulations
- Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced streamwise vorticity
- Three-dimensional coherent structures in a swirling jet undergoing vortex breakdown: stability analysis and empirical mode construction
- Helicity effects on inviscid instability in Batchelor vortices
- Topological structure of shock induced vortex breakdown
- Vortex breakdown in compressible flows in pipes
- Multistage interaction of a shock wave and a strong vortex
- Theory of the vortex breakdown phenomenon
- Interaction of a shock with a longitudinal vortex
- Numerical simulation of vortices with axial velocity deficits
- Three-dimensional vortex breakdown in swirling jets and wakes: direct numerical simulation
- Shock Wave—Turbulence Interactions
- The effect of compressibility on the critical swirl of vortex flows in a pipe
- On the identification of a vortex
- Enstrophy production and flow topology in compressible isotropic turbulence with vibrational non-equilibrium
- Converging near-elliptic shock waves
- Onset conditions for vortex breakdown in supersonic flows
- Reynolds- and Mach-number effects in canonical shock–turbulence interaction
- Axial flow in trailing line vortices
- Vortex Breakdown
- Dissipation and breakdown of a wing-tip vortex
- Three-dimensional simulations of large eddies in the compressible mixing layer
- Transition between regular and Mach reflection of shock waves: New numerical and experimental results
This page was built for publication: Streamwise vortex breakdown due to the interaction with crossed shock waves