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
Přednáška
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.
Klíčová slova anglicky
jet engine, exhaust gases temperature, glider, thermocouple
Vydáno
2018-05-14
Strany od–do
545–548
Počet stran
979
BIBTEX
@misc{BUT156015,
author="Jiří {Matějů}",
title="Temperature measurement behind self-sustaining jet engine of a glider",
year="2018",
pages="545--548"
}