Investigation of the effect of heavy gas injection into a supersonic boundary layer on laminar-turbulent transition

DOI10.1134/S0015462817060052zbMath1384.76047OpenAlexW2784546273MaRDI QIDQ1742456

A. A. Yatskikh, A. D. Kosinov, N. N. Zubkov, S. A. Gaponov, Yu. G. Ermolaev, V. I. Lysenko, Boris V. Smorodsky

Publication date: 11 April 2018

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0015462817060052

zbMATH Keywords

hydrodynamic stabilityinjectionlaminar-turbulent transitioncompressible boundary layerpermeable surface

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20) Transition to turbulence (76F06)

Cites Work

• Unnamed Item
• Joint permeability and roughness effect on the supersonic flat-plate boundary layer stability and transition
• Combined influence of coating permeability and roughness on supersonic boundary layer stability and transition

This page was built for publication: Investigation of the effect of heavy gas injection into a supersonic boundary layer on laminar-turbulent transition