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"
}