Physical Mechanism Underlying Symmetry Breaking of Shock Trains

No abstract is available for this paper.

• Publication year

  2025

• Venue

  AIAA Journal

• Publication date

  2025-08-18

• Fields of study

  Not labeled

• Identifiers
  DOI 10.2514/1.j065598
• External record

  Open on Semantic Scholar

• Source metadata

  Semantic Scholar

• No claims are published for this paper.

• No concepts are published for this paper.

• Asymmetries in Nominally Symmetric Flows

  2024cited by this paper
• Bi-global stability of supersonic backward-facing step flow

  2024cited by this paper
• Active noise control of a supersonic underexpanded planar jet guided by resolvent analysis

  2024cited by this paper
• BROADCAST: A high-order compressible CFD toolbox for stability and sensitivity using Algorithmic Differentiation

  2022cited by this paper
• Bifurcation scenario for a two-dimensional static airfoil exhibiting trailing edge stall

  2021cited by this paper
• Occurrence of global instability in hypersonic compression corner flow

  2021cited by this paper
• Influence of the inlet velocity profile on the flow stability in a symmetric channel expansion

  2020cited by this paper
• On the turbulence amplification in shock-wave/turbulent boundary layer interaction

  2020cited by this paper
• Theoretical Model and Numerical Analysis for Asymmetry of Shock Train in Supersonic Flows

  2020cited by this paper
• On the origin and propagation of perturbations that cause shock train inherent unsteadiness

  2018cited by this paper
• Global stability and control of the confined turbulent flow past a thick flat plate

  2017cited by this paper
• Quasi-laminar stability and sensitivity analyses for turbulent flows: Prediction of low-frequency unsteadiness and passive control

  2014cited by this paper
• Stability analysis and control of the flow in a symmetric channel with a sudden expansion

  2012cited by this paper
• Experimental and numerical analysis of the structure of pseudo-shock systems in laval nozzles with parallel side walls

  2010cited by this paper
• Supersonic flow separation in planar nozzles

  2009cited by this paper
• Stability of flow past a cylinder: Energy budget of eigenmodes

  2009cited by this paper
• Predicting the onset of flow unsteadiness based on global instability

  2007cited by this paper
• Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes

  1997cited by this paper
• A One-Equation Turbulence Model for Aerodynamic Flows

  1992cited by this paper
• Characteristics of multiple shock wave/turbulent boundary-layer interactions in rectangular ducts

  1990cited by this paper
• Lower-upper Symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations

  1988cited by this paper
• Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes

  1981cited by this paper
• Towards the ultimate conservative difference scheme V. A second-order sequel to Godunov's method

  1979cited by this paper

• Numerical investigation on the flow characteristics of shock trains in supersonic square-to-circular transition ducts

  2025cites this paper