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...

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Main Authors: Yerokhin Alexander, Deniskin Yury, Dubrovin Anton, Sheryshev Alexei
Format: Article
Language:English
Published: EDP Sciences 2023-01-01
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.
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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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