Numerical study of surface roughness effects in the boundary layer of a blunted cone in a supersonic flow
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http://aip.scitation.org/doi/pdf/10.1063/1.5065210
Reference9 articles.
1. Effects of Roughness on Hypersonic Boundary-Layer Transition
2. Roughness-Induced Instability in a Hypersonic Laminar Boundary Layer
3. Effect of the surface roughness of blunt cone forebody on the position of laminar-turbulent transition
4. Turbulization of the wake behind a single roughness element on a blunted body at a hypersonic Mach number
5. M. Choudhari, A. Norris, F. Li, C.-L. Chang, and J. Edwards, AIAA Paper 2013–0081 (2013).
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