Experimental Investigation of Three-Dimensional Supersonic Flow past an Axisymmetric Body with an Annular Cavityстатья
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Дата последнего поиска статьи во внешних источниках: 10 июня 2020 г.
Аннотация:The results of an experimental investigation of supersonic Mach 2.5 flow past an axisymmetric
cylindrical model body with a rectangular annular cut-out on its lateral surface are presented.
The evolution of the structure of the flow over the cavity with continuous variation in the angle of attack is studied on the basis of the data of flow visualization and balance measurements on the range of the relative cavity lengths L/h from 8 to 16. Hysteresis phenomena are revealed and analyzed. Keywords: hysteresis, supersonic flow, flow separation, annular cavity, angle of attack, aerodynamic
drag coefficient.