Detail publikace

Temperature measurement behind self-sustaining jet engine of a glider

MATĚJŮ, J.

Originální název

Temperature measurement behind self-sustaining jet engine of a glider

Typ

přednáška

Jazyk

angličtina

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

jet engine, exhaust gases temperature, glider, thermocouple

Autoři

MATĚJŮ, J.

Vydáno

14. 5. 2018

Strany od

545

Strany do

548

Strany počet

979

BibTex

@misc{BUT156015,
  author="Jiří {Matějů}",
  title="Temperature measurement behind self-sustaining jet engine of a glider",
  year="2018",
  pages="545--548",
  note="lecture"
}