Computer Engineering System Application for Calculating the Aerodynamic Characteristics of Cargo Separated from the Aircraft

<p>Ensuring the safety of the cargo separated from the aircraft is one of the most important criteria in the development of cargo transportation systems. The article shows that the experimental studies using wind tunnels are time- and cost-consuming. Therefore, at the early stages in designing...

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Main Authors: O. V. Korizhin, O. B. Paschenko, M. V. Filippov
Format: Article
Language:Russian
Published: MGTU im. N.È. Baumana 2014-01-01
Series:Nauka i Obrazovanie
Subjects:
CFD
CAD
CAE
Online Access:http://technomag.edu.ru/jour/article/view/739
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spelling doaj-3d1e363963174dc5ba5497e9a8c7d1372020-11-24T22:00:23ZrusMGTU im. N.È. BaumanaNauka i Obrazovanie1994-04082014-01-0101132032910.7463/1114.0739817739Computer Engineering System Application for Calculating the Aerodynamic Characteristics of Cargo Separated from the AircraftO. V. Korizhin0O. B. Paschenko1M. V. Filippov2Russian Aircraft Corporation "MiG", MoscowRussian Aircraft Corporation "MiG", MoscowBauman Moscow State Technical University, Moscow<p>Ensuring the safety of the cargo separated from the aircraft is one of the most important criteria in the development of cargo transportation systems. The article shows that the experimental studies using wind tunnels are time- and cost-consuming. Therefore, at the early stages in designing an aerodynamic configuration of the aircraft the software systems of solid modeling and computational fluid dynamics are, usually, used. The article describes the shortcomings of such software systems because of the large-scale computational costs. The offered technique for calculating the aerodynamic characteristics of cargo separated from the aircraft uses two main points. Firstly, in calculations a strategy of reducing a size of the grid cells when approaching to the object surface was used. Secondly, in modeling the trajectories of the separated cargo in the neibourhood of carrier aircraft a multivariate interpolation was used for prossessing the results of computational experiments and their subsequent applications.</p><p>The proposed technique allowed a significant reduction of the computational costs when determining the aerodynamic characteristics. This technique was used to evaluate a reliabiity of obtained results through their comparison with available experimental data.</p>http://technomag.edu.ru/jour/article/view/739aerodynamic characteristicssafety of separationcomputational fluid dynamicCFDCADCAEmultidimensional interpolationsolid modeling
collection DOAJ
language Russian
format Article
sources DOAJ
author O. V. Korizhin
O. B. Paschenko
M. V. Filippov
spellingShingle O. V. Korizhin
O. B. Paschenko
M. V. Filippov
Computer Engineering System Application for Calculating the Aerodynamic Characteristics of Cargo Separated from the Aircraft
Nauka i Obrazovanie
aerodynamic characteristics
safety of separation
computational fluid dynamic
CFD
CAD
CAE
multidimensional interpolation
solid modeling
author_facet O. V. Korizhin
O. B. Paschenko
M. V. Filippov
author_sort O. V. Korizhin
title Computer Engineering System Application for Calculating the Aerodynamic Characteristics of Cargo Separated from the Aircraft
title_short Computer Engineering System Application for Calculating the Aerodynamic Characteristics of Cargo Separated from the Aircraft
title_full Computer Engineering System Application for Calculating the Aerodynamic Characteristics of Cargo Separated from the Aircraft
title_fullStr Computer Engineering System Application for Calculating the Aerodynamic Characteristics of Cargo Separated from the Aircraft
title_full_unstemmed Computer Engineering System Application for Calculating the Aerodynamic Characteristics of Cargo Separated from the Aircraft
title_sort computer engineering system application for calculating the aerodynamic characteristics of cargo separated from the aircraft
publisher MGTU im. N.È. Baumana
series Nauka i Obrazovanie
issn 1994-0408
publishDate 2014-01-01
description <p>Ensuring the safety of the cargo separated from the aircraft is one of the most important criteria in the development of cargo transportation systems. The article shows that the experimental studies using wind tunnels are time- and cost-consuming. Therefore, at the early stages in designing an aerodynamic configuration of the aircraft the software systems of solid modeling and computational fluid dynamics are, usually, used. The article describes the shortcomings of such software systems because of the large-scale computational costs. The offered technique for calculating the aerodynamic characteristics of cargo separated from the aircraft uses two main points. Firstly, in calculations a strategy of reducing a size of the grid cells when approaching to the object surface was used. Secondly, in modeling the trajectories of the separated cargo in the neibourhood of carrier aircraft a multivariate interpolation was used for prossessing the results of computational experiments and their subsequent applications.</p><p>The proposed technique allowed a significant reduction of the computational costs when determining the aerodynamic characteristics. This technique was used to evaluate a reliabiity of obtained results through their comparison with available experimental data.</p>
topic aerodynamic characteristics
safety of separation
computational fluid dynamic
CFD
CAD
CAE
multidimensional interpolation
solid modeling
url http://technomag.edu.ru/jour/article/view/739
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AT obpaschenko computerengineeringsystemapplicationforcalculatingtheaerodynamiccharacteristicsofcargoseparatedfromtheaircraft
AT mvfilippov computerengineeringsystemapplicationforcalculatingtheaerodynamiccharacteristicsofcargoseparatedfromtheaircraft
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