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MATĚJŮ, J.
Originální název
Temperature measurement behind self-sustaining jet engine of a glider
Anglický název
Druh
Stať ve sborníku v databázi WoS či Scopus
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
Klíčová slova
jet engine, exhaust gases temperature, glider, thermocouple
Klíčová slova v angličtině
Autoři
Rok RIV
2019
Vydáno
14.05.2018
ISBN
978-80-86246-88-8
Kniha
ENGINEERING MECHANICS 2018
ISSN
1805-8248
Periodikum
Engineering Mechanics
Stát
Česká republika
Strany od
545
Strany do
548
Strany počet
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" }