Analyzes regarding aviation fuels parameters use on jet engines-Reference-Cited by-同舟云学术

Analyzes regarding aviation fuels parameters use on jet engines

Published:2024-06-10 Issue:2 Volume:16 Page:113-122
ISSN:2247-4528
Container-title:INCAS BULLETIN
language:en
Short-container-title:INCAS BULLETIN

Author:

PRISACARIU Vasile¹,ANDREI Irina²,MIHAI Eduard³

Affiliation:

1. “Henri Coandă” Air Force Academy, Brașov, Mihai Viteazul 160, Brașov, 500187, Romania, prisacariu.vasile@afahc.ro

2. INCAS – National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, andrei.irina@incas.ro

3. “Henri Coandă” Air Force Academy, Brașov, Mihai Viteazul 160, Brașov, 500187, Romania, eduard.mihai@afahc.ro

Abstract

The properties of the fuels determine the quality of the combustion process and implicitly the performance of the turbojet engine. The optimal heterogeneous combustion process of an aviation fuel is ensured by a stoichiometric ratio (fuel/fuel), a combustion temperature and a maximum loading degree of the combustion chamber. The article includes a numerical analysis instrumented with Gasturb software that highlights the influence of fuel quality and combustion process characteristics of a Rolls Royce Viper turbojet engine on its performance.

Publisher

INCAS - National Institute for Aerospace Research Elie Carafoli

Reference22 articles.

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