Determination of the operational parameters values for Airbus A300-600ST Beluga aircraft on the basis of CFD tests
The article presents a method for estimating the values of basic operational and aerodynamic parameters of an aircraft. It contains a multistage analysis of CFD test results for the Beluga Airbus A300-600ST model. The first step of the method is to determine the values of aerodynamic parameters such...
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Online Access: | https://doi.org/10.1051/matecconf/202235702019 https://doaj.org/article/ffbefc71a10d4b1fb33caff3112d53bc |
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ftdoajarticles:oai:doaj.org/article:ffbefc71a10d4b1fb33caff3112d53bc 2023-05-15T15:41:36+02:00 Determination of the operational parameters values for Airbus A300-600ST Beluga aircraft on the basis of CFD tests Nowacki Marcin Olejniczak Damian 2022-01-01T00:00:00Z https://doi.org/10.1051/matecconf/202235702019 https://doaj.org/article/ffbefc71a10d4b1fb33caff3112d53bc EN FR eng fre EDP Sciences https://www.matec-conferences.org/articles/matecconf/pdf/2022/04/matecconf_mms2020_02019.pdf https://doaj.org/toc/2261-236X 2261-236X doi:10.1051/matecconf/202235702019 https://doaj.org/article/ffbefc71a10d4b1fb33caff3112d53bc MATEC Web of Conferences, Vol 357, p 02019 (2022) Engineering (General). Civil engineering (General) TA1-2040 article 2022 ftdoajarticles https://doi.org/10.1051/matecconf/202235702019 2022-12-30T21:22:53Z The article presents a method for estimating the values of basic operational and aerodynamic parameters of an aircraft. It contains a multistage analysis of CFD test results for the Beluga Airbus A300-600ST model. The first step of the method is to determine the values of aerodynamic parameters such as lift coefficient, drag coefficient, lift force and drag force in specific flight conditions. A comparative analysis of the coefficients of lift and drag force depending on the angle of attack of the aircraft allowed the estimation of the optimal angle of attack of the Airbus A300-600ST Beluga. In the next step, the operational values and the maximum flight ceiling of the aircraft were determined. For this purpose, the results of CFD simulation tests for the optimal angle of attack of the aircraft were used. This article allowed determining the characteristics of the components of aerodynamic force of an airplane depending on the angle of attack, flight altitude and flight speed, determining the optimal angle of attack of the aircraft and calculation of the optimal and maximum flight ceiling values of the Airbus A300-600ST Beluga. Article in Journal/Newspaper Beluga Beluga* Directory of Open Access Journals: DOAJ Articles MATEC Web of Conferences 357 02019 |
institution |
Open Polar |
collection |
Directory of Open Access Journals: DOAJ Articles |
op_collection_id |
ftdoajarticles |
language |
English French |
topic |
Engineering (General). Civil engineering (General) TA1-2040 |
spellingShingle |
Engineering (General). Civil engineering (General) TA1-2040 Nowacki Marcin Olejniczak Damian Determination of the operational parameters values for Airbus A300-600ST Beluga aircraft on the basis of CFD tests |
topic_facet |
Engineering (General). Civil engineering (General) TA1-2040 |
description |
The article presents a method for estimating the values of basic operational and aerodynamic parameters of an aircraft. It contains a multistage analysis of CFD test results for the Beluga Airbus A300-600ST model. The first step of the method is to determine the values of aerodynamic parameters such as lift coefficient, drag coefficient, lift force and drag force in specific flight conditions. A comparative analysis of the coefficients of lift and drag force depending on the angle of attack of the aircraft allowed the estimation of the optimal angle of attack of the Airbus A300-600ST Beluga. In the next step, the operational values and the maximum flight ceiling of the aircraft were determined. For this purpose, the results of CFD simulation tests for the optimal angle of attack of the aircraft were used. This article allowed determining the characteristics of the components of aerodynamic force of an airplane depending on the angle of attack, flight altitude and flight speed, determining the optimal angle of attack of the aircraft and calculation of the optimal and maximum flight ceiling values of the Airbus A300-600ST Beluga. |
format |
Article in Journal/Newspaper |
author |
Nowacki Marcin Olejniczak Damian |
author_facet |
Nowacki Marcin Olejniczak Damian |
author_sort |
Nowacki Marcin |
title |
Determination of the operational parameters values for Airbus A300-600ST Beluga aircraft on the basis of CFD tests |
title_short |
Determination of the operational parameters values for Airbus A300-600ST Beluga aircraft on the basis of CFD tests |
title_full |
Determination of the operational parameters values for Airbus A300-600ST Beluga aircraft on the basis of CFD tests |
title_fullStr |
Determination of the operational parameters values for Airbus A300-600ST Beluga aircraft on the basis of CFD tests |
title_full_unstemmed |
Determination of the operational parameters values for Airbus A300-600ST Beluga aircraft on the basis of CFD tests |
title_sort |
determination of the operational parameters values for airbus a300-600st beluga aircraft on the basis of cfd tests |
publisher |
EDP Sciences |
publishDate |
2022 |
url |
https://doi.org/10.1051/matecconf/202235702019 https://doaj.org/article/ffbefc71a10d4b1fb33caff3112d53bc |
genre |
Beluga Beluga* |
genre_facet |
Beluga Beluga* |
op_source |
MATEC Web of Conferences, Vol 357, p 02019 (2022) |
op_relation |
https://www.matec-conferences.org/articles/matecconf/pdf/2022/04/matecconf_mms2020_02019.pdf https://doaj.org/toc/2261-236X 2261-236X doi:10.1051/matecconf/202235702019 https://doaj.org/article/ffbefc71a10d4b1fb33caff3112d53bc |
op_doi |
https://doi.org/10.1051/matecconf/202235702019 |
container_title |
MATEC Web of Conferences |
container_volume |
357 |
container_start_page |
02019 |
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1766374492192374784 |