Detail publikace

Temperature measurement behind self-sustaining jet engine of a glider

MATĚJŮ, J.

Anglický název

Temperature measurement behind self-sustaining jet engine of a glider

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

en

Originální abstrakt

Analysis of temperature field behind a small jet engine TBS400N-TJ42 was necessary for finding the maximum temperature of exhaust gases mainly at a glider tail position. Results can be useful for validating simulation tool. A low cost 1-axis manual traverse system with 9 K-type thermocouples was made for this purpose. The maximum temperature at the tail position was less than 83 °C ± 2.5 °C during static tests. Many HpH flight tests showed maximum temperature of 65 °C on the tail of an aircraft. The composite tail technology of production was modified for higher temperature endurance.

Anglický abstrakt

Analysis of temperature field behind a small jet engine TBS400N-TJ42 was necessary for finding the maximum temperature of exhaust gases mainly at a glider tail position. Results can be useful for validating simulation tool. A low cost 1-axis manual traverse system with 9 K-type thermocouples was made for this purpose. The maximum temperature at the tail position was less than 83 °C ± 2.5 °C during static tests. Many HpH flight tests showed maximum temperature of 65 °C on the tail of an aircraft. The composite tail technology of production was modified for higher temperature endurance.

Klíčová slova anglicky

jet engine, exhaust gases temperature, glider, thermocouple

Vydáno

14.05.2018

ISBN

978-80-86246-88-8

ISSN

1805-8248

Kniha

ENGINEERING MECHANICS 2018

Strany od–do

545–548

Počet stran

979

BIBTEX


@inproceedings{BUT151316,
  author="Jiří {Matějů},
  title="Temperature measurement behind self-sustaining jet engine of a glider",
  booktitle="ENGINEERING MECHANICS 2018",
  year="2018",
  month="May",
  pages="545--548",
  isbn="978-80-86246-88-8",
  issn="1805-8248"
}