Interactions between vortical, acoustic and thermal components during hypersonic transition
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Publication:5742310
DOI10.1017/JFM.2019.176zbMath1415.76431OpenAlexW2939650934MaRDI QIDQ5742310
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Publication date: 14 May 2019
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/jfm.2019.176
Nonlinear effects in hydrodynamic stability (76E30) Shear flows and turbulence (76F10) Hydro- and aero-acoustics (76Q05) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)
Related Items (5)
Effect of flow–thermodynamics interactions on the stability of compressible boundary layers: insights from Helmholtz decomposition ⋮ Growth mechanisms of second-mode instability in hypersonic boundary layers ⋮ Optimal heat flux for delaying transition to turbulence in a high-speed boundary layer ⋮ First-mode-induced nonlinear breakdown in a hypersonic boundary layer ⋮ Instabilities and transition in cooled wall hypersonic boundary layers
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