Velocity and Temperature Profile Analyzes in Supersonic Flow in the Experimental System

This article deals with the preparation of the experimental chamber on which, among other things, stagnation and static temperature will be measured. The results obtained from the measurements will be compared with the results of mathematical-physics analyzes of the Ansys Fluent system. Analyzes of the expected stagnation temperatures at the tip of the probes were performed with respect to the course of the Mach number from the aperture.