A note on the appearance of wave-packets in steady-state triple-deck solutions of supersonic flow past a compression corner
DOI10.1017/jfm.2022.955zbMath1503.76082OpenAlexW4310555666MaRDI QIDQ5056283
A. J. Neely, D. Exposito, S. L. Gai
Publication date: 7 December 2022
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/jfm.2022.955
second-order finite difference schemeboundary layer separationChebyshev collocation pointcorner discontinuityNewton linearisation
Finite difference methods applied to problems in fluid mechanics (76M20) Asymptotic methods, singular perturbations applied to problems in fluid mechanics (76M45) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)
Uses Software
Cites Work
- Theory of laminar boundary layer separation in supersonic flow
- A semi–direct method for calculating flows with viscous–inviscid interaction
- Instability of supersonic compression ramp flow
- Inviscid–viscous interaction on triple-deck scales in a hypersonic flow with strong wall cooling
- On the stability and the numerical solution of the unsteady interactive boundary-layer equation
- Finite‐time break‐up can occur in any unsteady interacting boundary layer
- A reversed-flow singularity in interacting boundary layers
- Numerical solution of the local asymptotic problem of the unsteady separation of a laminar boundary layer in a supersonic flow
- The interactive breakdown in supersonic ramp flow
- On the non-parallel flow stability of the Blasius boundary layer
- The influence of wall cooling on hypersonic boundary-layer separation and stability
- Instabilities in supersonic compression ramp flow
- Once again on the supersonic flow separation near a corner
- An instability in supersonic boundary-layer flow over a compression ramp
- Self-induced separation
- Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
- On supersonic laminar boundary layers near convex corners
- Fluid Dynamics
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