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

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26220%2F21%3APU138337" target="_blank" >RIV/00216305:26220/21:PU138337 - isvavai.cz</a>
Výsledek na webu
<a href="https://iopscience.iop.org/article/10.1149/09901.0325ecst/pdf" target="_blank" >https://iopscience.iop.org/article/10.1149/09901.0325ecst/pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1149/09901.0325ecst" target="_blank" >10.1149/09901.0325ecst</a>

Jazyk výsledku
angličtina
Název v původním jazyce
Velocity and Temperature Profile Analyzes in Supersonic Flow in the Experimental System
Popis výsledku v původním jazyce
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.
Název v anglickém jazyce
Velocity and Temperature Profile Analyzes in Supersonic Flow in the Experimental System
Popis výsledku anglicky
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.

Rok uplatnění
2021
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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