Airfoil smoothing using unconditional optimization taking into account aerodynamic criteria
The smoothing of airfoils in sections of the surface of an aircraft wing is considered. The issue of using the distribution of pressure and Mach number along the chord of an airfoil as criteria for smoothing efficiency is being studied. Smoothing is considered as a problem of unconditional minimizat...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
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EDP Sciences
2023-01-01
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Series: | E3S Web of Conferences |
Online Access: | https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/97/e3sconf_bft2023_07021.pdf |
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author | Yerokhin Alexander Deniskin Yury Dubrovin Anton Sheryshev Alexei |
author_facet | Yerokhin Alexander Deniskin Yury Dubrovin Anton Sheryshev Alexei |
author_sort | Yerokhin Alexander |
collection | DOAJ |
description | The smoothing of airfoils in sections of the surface of an aircraft wing is considered. The issue of using the distribution of pressure and Mach number along the chord of an airfoil as criteria for smoothing efficiency is being studied. Smoothing is considered as a problem of unconditional minimization of a quadratic objective function. The arguments of the objective function are the second derivatives of the tabular function interpolating the contour of the airfoil. Minimization is performed using the gradient descent method. |
first_indexed | 2024-03-08T11:14:33Z |
format | Article |
id | doaj.art-95885b21028142d4a4fb54cf49990143 |
institution | Directory Open Access Journal |
issn | 2267-1242 |
language | English |
last_indexed | 2024-03-08T11:14:33Z |
publishDate | 2023-01-01 |
publisher | EDP Sciences |
record_format | Article |
series | E3S Web of Conferences |
spelling | doaj.art-95885b21028142d4a4fb54cf499901432024-01-26T10:38:31ZengEDP SciencesE3S Web of Conferences2267-12422023-01-014600702110.1051/e3sconf/202346007021e3sconf_bft2023_07021Airfoil smoothing using unconditional optimization taking into account aerodynamic criteriaYerokhin Alexander0Deniskin Yury1Dubrovin Anton2Sheryshev Alexei3Moscow Aviation Institute (National Research University)Moscow Aviation Institute (National Research University)Moscow Aviation Institute (National Research University)Moscow Aviation Institute (National Research University)The smoothing of airfoils in sections of the surface of an aircraft wing is considered. The issue of using the distribution of pressure and Mach number along the chord of an airfoil as criteria for smoothing efficiency is being studied. Smoothing is considered as a problem of unconditional minimization of a quadratic objective function. The arguments of the objective function are the second derivatives of the tabular function interpolating the contour of the airfoil. Minimization is performed using the gradient descent method.https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/97/e3sconf_bft2023_07021.pdf |
spellingShingle | Yerokhin Alexander Deniskin Yury Dubrovin Anton Sheryshev Alexei Airfoil smoothing using unconditional optimization taking into account aerodynamic criteria E3S Web of Conferences |
title | Airfoil smoothing using unconditional optimization taking into account aerodynamic criteria |
title_full | Airfoil smoothing using unconditional optimization taking into account aerodynamic criteria |
title_fullStr | Airfoil smoothing using unconditional optimization taking into account aerodynamic criteria |
title_full_unstemmed | Airfoil smoothing using unconditional optimization taking into account aerodynamic criteria |
title_short | Airfoil smoothing using unconditional optimization taking into account aerodynamic criteria |
title_sort | airfoil smoothing using unconditional optimization taking into account aerodynamic criteria |
url | https://www.e3s-conferences.org/articles/e3sconf/pdf/2023/97/e3sconf_bft2023_07021.pdf |
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