Publication detail
Temperature measurement behind self-sustaining jet engine of a glider
MATĚJŮ, J.
English title
Temperature measurement behind self-sustaining jet engine of a glider
Type
Paper in proceedings (conference paper)
Language
en
Original abstract
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.
Keywords in English
jet engine, exhaust gases temperature, glider, thermocouple
Released
2018-05-14
ISBN
978-80-86246-88-8
ISSN
1805-8248
Book
ENGINEERING MECHANICS 2018
Pages from–to
545–548
Pages count
979
BIBTEX
@inproceedings{BUT151316,
author="Jiří {Matějů}",
title="Temperature measurement behind self-sustaining jet engine of a glider",
booktitle="ENGINEERING MECHANICS 2018",
year="2018",
journal="Engineering Mechanics",
pages="545--548",
doi="10.21495/91-8-545",
isbn="978-80-86246-88-8",
issn="1805-8248"
}