Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability
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http://aip.scitation.org/doi/pdf/10.1063/1.5065361
Reference13 articles.
1. Combined influence of coating permeability and roughness on supersonic boundary layer stability and transition
2. The Hot-Wire Anemometer in Supersonic Flow
3. Experimental determination of the free-stream disturbance field in a short-duration supersonic wind tunnel
4. Constant temperature hot-wire measurements in a short duration supersonic wind tunnel
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1. Experimental study of the disturbances development in the boundary layer of a flat plate with a wavy surface at supersonic flow;ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS;2023
2. Experimental studies of pulsations of the boundary layer of swept wings with periodic roughness at M = 4;ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS;2023
3. Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer at Mach 2-4;AIP Conference Proceedings;2021
4. Experimental investigation of the natural and controlled disturbance development in a supersonic boundary layer on the swept wing;Journal of Physics: Conference Series;2019-11-01
5. The controlled periodic impact on the longitudinal vortex in the boundary layer at Mach 2;Journal of Physics: Conference Series;2019-11-01
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