Response of a hypersonic turbulent boundary layer to favourable pressure gradients

DOI10.1017/jfm.2013.89zbMath1287.76026OpenAlexW2334091394MaRDI QIDQ5417311

N. R. Tichenor, Raymond A. Humble, Rodney D. W. Bowersox

Publication date: 21 May 2014

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2013.89

zbMATH Keywords

turbulent boundary layerhypersonicfavourable pressure gradient

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Turbulent boundary layers (76F40) Hypersonic flows (76K05)

Related Items

Resolution effects in compressible, turbulent boundary layer simulations ⋮ Small perturbation evolution in compressible Poiseuille flow: pressure–velocity interactions and obliqueness effects ⋮ The amplification of large-scale motion in a supersonic concave turbulent boundary layer and its impact on the mean and statistical properties ⋮ Turbulence structures and statistics of a supersonic turbulent boundary layer subjected to concave surface curvature ⋮ Resolvent-based study of compressibility effects on supersonic turbulent boundary layers ⋮ Self-similar compressible turbulent boundary layers with pressure gradients. Part 1. Direct numerical simulation and assessment of Morkovin’s hypothesis ⋮ Direct numerical simulation of hypersonic turbulent boundary layers: effect of spatial evolution and Reynolds number

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