Dobrov Y.V. , Lashkov V.A. , Mashek I.Ch. , Khoronzhuk R.S

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_13701094

This work devoted to the investigation of effects that occur after local energy deposition in front of a well-streamlined body in supersonic flow. Local energy deposition was produced using an interelectrode direct current discharge. Under a well-streamlined body, one is assumed a wedge with apex angle of about 14 degrees. We carried out numerical calculations and experimental studies of interaction between the gas region, which heated by discharge, with a shock wave on the body. As a result of interaction, a strong change in the nature of flow near the body was observed.

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In Categories: Aerodynamics, High-Speed Aerodynamics and Aerothermodynamics, HiSST 2018, Hypersonic Aerodynamics, Hypersonic Fundamentals and History, Testing and Evaluation
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