Analysis of Avgas Fuel Spraying Schemes Using the ANSYS Application Approach

Avgas fuel consumption on Cessna trainer aircraft is very high. However, there has been little research regarding spray impacts in Cessna aircraft engines. The phenomenon of avgas spray colliding with the cylinder wall may occur during fuel injection, resulting in a changed spray radius and height,...

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Main Authors: Dimas Endrawan Putra, Nasrul Ilminnafik, M Fahrur Rozy Hentihu, Muh. Nurkoyim Kustanto, Danang Yudistiro, Skriptyan N.H. Syuhri
Format: Article
Language:English
Published: Universitas Negeri Malang 2024-05-01
Series:Journal of Mechanical Engineering Science and Technology
Subjects:
Online Access:https://journal2.um.ac.id/index.php/jmest/article/view/48417
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author Dimas Endrawan Putra
Nasrul Ilminnafik
M Fahrur Rozy Hentihu
Muh. Nurkoyim Kustanto
Danang Yudistiro
Skriptyan N.H. Syuhri
author_facet Dimas Endrawan Putra
Nasrul Ilminnafik
M Fahrur Rozy Hentihu
Muh. Nurkoyim Kustanto
Danang Yudistiro
Skriptyan N.H. Syuhri
author_sort Dimas Endrawan Putra
collection DOAJ
description Avgas fuel consumption on Cessna trainer aircraft is very high. However, there has been little research regarding spray impacts in Cessna aircraft engines. The phenomenon of avgas spray colliding with the cylinder wall may occur during fuel injection, resulting in a changed spray radius and height, which will affect the mixing of fuel and air. In several aspects, this affects engine performance and exhaust emissions on Cessna aircraft. This research aims to determine and study the phenomenon of spray impact on avgas-fueled aircraft engines. The fuel spray in the study occurred in the combustion chamber using pressure from a fuel hand pump whose pressure was supplied from a compressor with a pressure adjusted to the original pressure on the aircraft, namely 2 Bar (30 Psi). The experiments in this research used a high-speed camera system to study the phenomenon of avgas spray on walls to get better spray distribution. The results of this research were processed using the CFD application. The result of this research is that the greater the pressure, the more concentrated the resulting jet will be on the jet wall so that the atomization of the fuel jet will be dispersed. When the burst occurs, a change of 3.80e+00 occurs compared to other burst pressures.
format Article
id doaj-art-d7568e6162ec446d8c4b707cbb22a6ce
institution Kabale University
issn 2580-0817
2580-2402
language English
publishDate 2024-05-01
publisher Universitas Negeri Malang
record_format Article
series Journal of Mechanical Engineering Science and Technology
spelling doaj-art-d7568e6162ec446d8c4b707cbb22a6ce2025-02-04T00:25:57ZengUniversitas Negeri MalangJournal of Mechanical Engineering Science and Technology2580-08172580-24022024-05-0181718110.17977/um016v8i12024p07111357Analysis of Avgas Fuel Spraying Schemes Using the ANSYS Application ApproachDimas Endrawan Putra0Nasrul Ilminnafik1M Fahrur Rozy Hentihu2Muh. Nurkoyim KustantoDanang YudistiroSkriptyan N.H. Syuhriuniversitas negeri JemberUniversitas JemberUniversitas JemberAvgas fuel consumption on Cessna trainer aircraft is very high. However, there has been little research regarding spray impacts in Cessna aircraft engines. The phenomenon of avgas spray colliding with the cylinder wall may occur during fuel injection, resulting in a changed spray radius and height, which will affect the mixing of fuel and air. In several aspects, this affects engine performance and exhaust emissions on Cessna aircraft. This research aims to determine and study the phenomenon of spray impact on avgas-fueled aircraft engines. The fuel spray in the study occurred in the combustion chamber using pressure from a fuel hand pump whose pressure was supplied from a compressor with a pressure adjusted to the original pressure on the aircraft, namely 2 Bar (30 Psi). The experiments in this research used a high-speed camera system to study the phenomenon of avgas spray on walls to get better spray distribution. The results of this research were processed using the CFD application. The result of this research is that the greater the pressure, the more concentrated the resulting jet will be on the jet wall so that the atomization of the fuel jet will be dispersed. When the burst occurs, a change of 3.80e+00 occurs compared to other burst pressures.https://journal2.um.ac.id/index.php/jmest/article/view/48417avgas, ansys, cfd, impigment, spray
spellingShingle Dimas Endrawan Putra
Nasrul Ilminnafik
M Fahrur Rozy Hentihu
Muh. Nurkoyim Kustanto
Danang Yudistiro
Skriptyan N.H. Syuhri
Analysis of Avgas Fuel Spraying Schemes Using the ANSYS Application Approach
Journal of Mechanical Engineering Science and Technology
avgas, ansys, cfd, impigment, spray
title Analysis of Avgas Fuel Spraying Schemes Using the ANSYS Application Approach
title_full Analysis of Avgas Fuel Spraying Schemes Using the ANSYS Application Approach
title_fullStr Analysis of Avgas Fuel Spraying Schemes Using the ANSYS Application Approach
title_full_unstemmed Analysis of Avgas Fuel Spraying Schemes Using the ANSYS Application Approach
title_short Analysis of Avgas Fuel Spraying Schemes Using the ANSYS Application Approach
title_sort analysis of avgas fuel spraying schemes using the ansys application approach
topic avgas, ansys, cfd, impigment, spray
url https://journal2.um.ac.id/index.php/jmest/article/view/48417
work_keys_str_mv AT dimasendrawanputra analysisofavgasfuelsprayingschemesusingtheansysapplicationapproach
AT nasrulilminnafik analysisofavgasfuelsprayingschemesusingtheansysapplicationapproach
AT mfahrurrozyhentihu analysisofavgasfuelsprayingschemesusingtheansysapplicationapproach
AT muhnurkoyimkustanto analysisofavgasfuelsprayingschemesusingtheansysapplicationapproach
AT danangyudistiro analysisofavgasfuelsprayingschemesusingtheansysapplicationapproach
AT skriptyannhsyuhri analysisofavgasfuelsprayingschemesusingtheansysapplicationapproach