Correction of the Supersonic Flow Impact on the Results of the Inserted Temperature Probe in the Differentially Pumped Chamber

Abstract

This article deals with the experimental chamber preparation, on which stagnation and static temperature (besides others) will be measured. The results obtained from measurement will be compared with the results from mathematical – physics analysis of Ansys Fluent system and in this system, the temperature running and expected ratios for planned experimental measuring also will be mapped in the supersonic flow in the experimental chambers.