Correction of the supersonic flow impact on the results of the inserted temperature probe in the differentially pumped chamber.

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26220%2F19%3APU133690" target="_blank" >RIV/00216305:26220/19:PU133690 - isvavai.cz</a>
Výsledek na webu
<a href="https://ur.booksc.eu/book/79701503/233132" target="_blank" >https://ur.booksc.eu/book/79701503/233132</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1149/09501.0491ecst" target="_blank" >10.1149/09501.0491ecst</a>

Jazyk výsledku
angličtina
Název v původním jazyce
Correction of the supersonic flow impact on the results of the inserted temperature probe in the differentially pumped chamber.
Popis výsledku v původním jazyce
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.
Název v anglickém jazyce
Correction of the supersonic flow impact on the results of the inserted temperature probe in the differentially pumped chamber.
Popis výsledku anglicky
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.

Rok uplatnění
2019
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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