Numerical investigation of the nonlinear transition regime in a Mach 2 boundary layer
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Publication:3097673
DOI10.1017/S0022112010004556zbMath1225.76146OpenAlexW2169676798MaRDI QIDQ3097673
Stefan Wernz, Christian S. J. Mayer, Hermann F. Fasel
Publication date: 10 November 2011
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/s0022112010004556
Finite difference methods applied to problems in fluid mechanics (76M20) Boundary-layer theory for compressible fluids and gas dynamics (76N20) Transition to turbulence (76F06)
Related Items (6)
Three-dimensional turbulent supersonic flow over a plate ⋮ Effect of cone rotation on the nonlinear evolution of Mack modes in supersonic boundary layers ⋮ Principle of fundamental resonance in hypersonic boundary layers: an asymptotic viewpoint ⋮ Control of oblique-type breakdown in a supersonic boundary layer employing streaks ⋮ Nonlinear transition mechanism on a blunt cone at Mach 6: oblique breakdown ⋮ Control of oblique breakdown in a supersonic boundary layer employing a local cooling strip
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