Experimental study of natural disturbances of a supersonic boundary layer on a swept-wing model with periodic roughness

This article is devoted to the experimental study of perturbations in a modulated swept-wing boundary layer at Mach 2. The modulation of the boundary layer was created using periodic roughness of the surface of the experimental model. The mean flow and pulsations were measured using a hot-wire anemo...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Yatskikh, A. A., Panina, A. V., Yermolaev, Yu. G., Kosinov, A. D., Semionov, N. V.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Disturbances Frequency spectrum Modulation Roughness Spectrum analysis Supersonic boundary layers Swept wings
Online-Zugang:	Volltext
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