Correlation-regression models for calculating the weight of small-scale aircraft gas turbine engines

Several new correlation-regression models of weight calculation for small-scale aircraft gas turbine engines are proposed for their conceptual design stage. A comparison of the obtained weight models with each other and with the Kuz’michev model is carried out. Based on the obtained results, conclus...

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Main Authors: Filinov Evgeny, Kolmakova Daria, Avdeev Sergey, Krasilnikov Sergey
Format: Article
Language:English
Published: EDP Sciences 2018-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201822003004
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spelling doaj-18b9c4f18b6b4bb8b5e93c6a26c98a2b2021-02-02T08:18:42ZengEDP SciencesMATEC Web of Conferences2261-236X2018-01-012200300410.1051/matecconf/201822003004matecconf_icmsc2018_03004Correlation-regression models for calculating the weight of small-scale aircraft gas turbine enginesFilinov Evgeny0Kolmakova Daria1Avdeev Sergey2Krasilnikov Sergey3Samara National Research University, Department of Aircraft Engine TheorySamara National Research University, Department of Aircraft Engine TheorySamara National Research University, Department of Aircraft Engine TheorySamara National Research University, Department of Aircraft Engine TheorySeveral new correlation-regression models of weight calculation for small-scale aircraft gas turbine engines are proposed for their conceptual design stage. A comparison of the obtained weight models with each other and with the Kuz’michev model is carried out. Based on the obtained results, conclusions about the feasibility and scope of their application are drawn. New correlation-regression models differ from each other in the number of input parameters, as well as in the accuracy of forecasting the weight. In the course of the work, a database of main data and thermodynamic parameters of turbofan engines (TFE) is created consisting of 92 small-scale TFEs with thrust less than 50 kN. Based on the collected statistics, formulas were obtained that allow calculating the weight at the initial stage of engine design. The error in calculating the weight by these models is in range from 10% to 30%.https://doi.org/10.1051/matecconf/201822003004
collection DOAJ
language English
format Article
sources DOAJ
author Filinov Evgeny
Kolmakova Daria
Avdeev Sergey
Krasilnikov Sergey
spellingShingle Filinov Evgeny
Kolmakova Daria
Avdeev Sergey
Krasilnikov Sergey
Correlation-regression models for calculating the weight of small-scale aircraft gas turbine engines
MATEC Web of Conferences
author_facet Filinov Evgeny
Kolmakova Daria
Avdeev Sergey
Krasilnikov Sergey
author_sort Filinov Evgeny
title Correlation-regression models for calculating the weight of small-scale aircraft gas turbine engines
title_short Correlation-regression models for calculating the weight of small-scale aircraft gas turbine engines
title_full Correlation-regression models for calculating the weight of small-scale aircraft gas turbine engines
title_fullStr Correlation-regression models for calculating the weight of small-scale aircraft gas turbine engines
title_full_unstemmed Correlation-regression models for calculating the weight of small-scale aircraft gas turbine engines
title_sort correlation-regression models for calculating the weight of small-scale aircraft gas turbine engines
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2018-01-01
description Several new correlation-regression models of weight calculation for small-scale aircraft gas turbine engines are proposed for their conceptual design stage. A comparison of the obtained weight models with each other and with the Kuz’michev model is carried out. Based on the obtained results, conclusions about the feasibility and scope of their application are drawn. New correlation-regression models differ from each other in the number of input parameters, as well as in the accuracy of forecasting the weight. In the course of the work, a database of main data and thermodynamic parameters of turbofan engines (TFE) is created consisting of 92 small-scale TFEs with thrust less than 50 kN. Based on the collected statistics, formulas were obtained that allow calculating the weight at the initial stage of engine design. The error in calculating the weight by these models is in range from 10% to 30%.
url https://doi.org/10.1051/matecconf/201822003004
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AT kolmakovadaria correlationregressionmodelsforcalculatingtheweightofsmallscaleaircraftgasturbineengines
AT avdeevsergey correlationregressionmodelsforcalculatingtheweightofsmallscaleaircraftgasturbineengines
AT krasilnikovsergey correlationregressionmodelsforcalculatingtheweightofsmallscaleaircraftgasturbineengines
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