Object

Alternative title:

Analiza emisji tlenków azotu z wykorzystaniem oprogramowania GasTurb dla lotniczego silnika turbinowego F100-PW-229

Contributor:

Aleksandra LUDWICZAK

Abstract:

The article discusses various aspects related to determining the composition of exhaust gases (i.e. nitrogen oxides) generated by a turbine aircraft engine. The paper highlights the problem of ozone depletion caused by toxic components of aircraft engine exhaust gases. The study is concerned with an engine used on the F-16 aircraft, i.e. F100-PW-229. GasTurb 12 software was used to calculate the engine’s operating parameters and to determine nitrogen oxides emission levels. The calculations were also performed analytically. The calculated thrust value was compared with data published in scientific articles (thrust of the engine). Characteristics of NOx emissions were obtained as a function of high-pressure rotor speed, temperature at the combustion chamber outlet, temperature downstream of the compressor, and engine thrust. The results obtained seem to correlate closely with data available in the literature.

Place of publishing:

Warszawa

Publisher:

Wojskowa Akademia Techniczna

Date created:

2010 r.0

Date submitted:

2024-06-30

Date accepted:

2025-01-09

Date issued:

2025-03-31

Extent:

B5

Identifier:

oai:ribes-88.man.poznan.pl:2728

Call number:

doi:10.5604/01.3001.0055.0333

Electronic ISSN:

2720-5266

Print ISSN:

2081-5891

Language:

angielski

License:

click here to follow the link

Rights holder:

Wojskowa Akademia Techniczna

Starting page:

9

Ending page:

20

Volume:

16

Journal:

PROMECH

Keywords:

aircraft turbine engine, combustion chamber, exhaust gases, emissions, nitrogen oxides