Abstract
The study of the interaction of conical bodies with an incident supersonic flow is carried out. In the presented theoretical and experimental studies, the parameters of the incident flow near the investigated bodies were determined at different Mach numbers. Experimental studies were carried out using a supersonic atmospheric-vacuum tube of the aerodynamic laboratory of the Mozhaysky Military Space Academy. The theoretical study is based on the model of a viscous perfect gas described by the Navier-Stokes equations.
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