Investigation of Aerodynamic Characteristics of Aircrafts in a Rarefied Gas Flow Using the Moment Method

A one-dimensional nonstationary nonlinear moment system of equations and an approximation of Maxwell’s microscopic boundary condition will be introduced. The flight speed and surface temperature of the aircraft are included in the moment system of equations as coefficients. Macroscopic boundary cond...

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Main Authors: Auzhan Sakabekov, Saltanat Madaliyeva, Ryskul Yergazina
Format: Article
Language:English
Published: Wiley 2022-01-01
Series:International Journal of Mathematics and Mathematical Sciences
Online Access:http://dx.doi.org/10.1155/2022/6943602
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author Auzhan Sakabekov
Saltanat Madaliyeva
Ryskul Yergazina
author_facet Auzhan Sakabekov
Saltanat Madaliyeva
Ryskul Yergazina
author_sort Auzhan Sakabekov
collection DOAJ
description A one-dimensional nonstationary nonlinear moment system of equations and an approximation of Maxwell’s microscopic boundary condition will be introduced. The flight speed and surface temperature of the aircraft are included in the moment system of equations as coefficients. Macroscopic boundary conditions also depend on the surface temperature of the aircraft. The quantity of macroscopic boundary conditions for the moment system of equations depends on the parity of the approximation number of the moment system of equations. We state the initial and boundary value problem for the moment system of equations in the third approximation under macroscopic boundary conditions. This paper proves the existence and uniqueness of the solution of the abovementioned problem in the space of functions continuous in time and summable in the square by spatial variable. The theorem on the existence and uniqueness of a solution of the initial and boundary value problem for the moment system of equations in the third approximation is proved by the method of a priori estimation and using the Galerkin method and Tartar’s compensated compactness method.
format Article
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institution Kabale University
issn 1687-0425
language English
publishDate 2022-01-01
publisher Wiley
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series International Journal of Mathematics and Mathematical Sciences
spelling doaj-art-e3ae297bef7a422c9d86761e218eb1332025-02-03T05:53:49ZengWileyInternational Journal of Mathematics and Mathematical Sciences1687-04252022-01-01202210.1155/2022/6943602Investigation of Aerodynamic Characteristics of Aircrafts in a Rarefied Gas Flow Using the Moment MethodAuzhan Sakabekov0Saltanat Madaliyeva1Ryskul Yergazina2Satbayev UniversitySatbayev UniversitySatbayev UniversityA one-dimensional nonstationary nonlinear moment system of equations and an approximation of Maxwell’s microscopic boundary condition will be introduced. The flight speed and surface temperature of the aircraft are included in the moment system of equations as coefficients. Macroscopic boundary conditions also depend on the surface temperature of the aircraft. The quantity of macroscopic boundary conditions for the moment system of equations depends on the parity of the approximation number of the moment system of equations. We state the initial and boundary value problem for the moment system of equations in the third approximation under macroscopic boundary conditions. This paper proves the existence and uniqueness of the solution of the abovementioned problem in the space of functions continuous in time and summable in the square by spatial variable. The theorem on the existence and uniqueness of a solution of the initial and boundary value problem for the moment system of equations in the third approximation is proved by the method of a priori estimation and using the Galerkin method and Tartar’s compensated compactness method.http://dx.doi.org/10.1155/2022/6943602
spellingShingle Auzhan Sakabekov
Saltanat Madaliyeva
Ryskul Yergazina
Investigation of Aerodynamic Characteristics of Aircrafts in a Rarefied Gas Flow Using the Moment Method
International Journal of Mathematics and Mathematical Sciences
title Investigation of Aerodynamic Characteristics of Aircrafts in a Rarefied Gas Flow Using the Moment Method
title_full Investigation of Aerodynamic Characteristics of Aircrafts in a Rarefied Gas Flow Using the Moment Method
title_fullStr Investigation of Aerodynamic Characteristics of Aircrafts in a Rarefied Gas Flow Using the Moment Method
title_full_unstemmed Investigation of Aerodynamic Characteristics of Aircrafts in a Rarefied Gas Flow Using the Moment Method
title_short Investigation of Aerodynamic Characteristics of Aircrafts in a Rarefied Gas Flow Using the Moment Method
title_sort investigation of aerodynamic characteristics of aircrafts in a rarefied gas flow using the moment method
url http://dx.doi.org/10.1155/2022/6943602
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AT saltanatmadaliyeva investigationofaerodynamiccharacteristicsofaircraftsinararefiedgasflowusingthemomentmethod
AT ryskulyergazina investigationofaerodynamiccharacteristicsofaircraftsinararefiedgasflowusingthemomentmethod