Publication detail

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

ŠABACKÁ, P. MAXA, J. VYROUBAL, P.

Original Title

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

English Title

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

Type

conference paper

Language

en

Original 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.

English 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.

Keywords

Ansys, temperature probe, Differentialy pumped chamber.

Released

17.10.2019

ISBN

978-80-214-5109-4

Book

ABAF 20th issue of ECS Transactions

Pages from

100

Pages to

105

Pages count

6

BibTex


@inproceedings{BUT159308,
  author="Pavla {Šabacká} and Jiří {Maxa} and Petr {Vyroubal}",
  title="Correction of the supersonic flow impact on the results of the inserted temperature probe in the differentially pumped chamber.",
  annote="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.",
  booktitle="ABAF 20th issue of ECS Transactions",
  chapter="159308",
  howpublished="online",
  year="2019",
  month="october",
  pages="100--105",
  type="conference paper"
}