Abstract
Characteristics of the fields of mean density and density fluctuations measured with introduction of periodic disturbances into a hypersonic viscous boundary layer on a flat plate are presented. The experiments are performed for a flow Mach number M∞ = 21, Reynolds number per meter Re1∞ = 6·105 m−1, and temperature factor of the surface T w /T 0 = 0.26. The disturbances are introduced into the shock layer by an oblique gasdynamic whistle.
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