Determination of the density of molecular flows falling on a body of arbitrary shape under conditions of free-molecular flow

Aim. The aim of this work was to develop an algorithm for determining the density of incident mass, momentum and energy flows on a body of complex shape, flown around by a highly rarefied gas. Methodology. The work uses methods of the molecular-kinetic theory of gases, aimed at determining the macroscopic characteristics of a rarefied gas flow. The work is based on the numerical solution of integrals of the Maxwell distribution function. Results. An algorithm has been developed and tested on a model simulating a device (solar battery panel, antenna, etc.) installed on the surface of a spacecraft body. Research implications . The developed algorithm can be used in problems related to determining the distribution of mass, momentum and energy flow densities over the surface of objects flown around by a highly rarefied gas medium, and in problems related to determining the characteristics of a spacecraft's own external atmosphere.

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Publication Details

Journal
Bulletin of Federal State University of Education Series Physics and Mathematics
Published
2024-12-04
DOI
https://doi.org/10.18384/2949-5067-2024-3-33-49
Primary Topic
Gas Dynamics and Kinetic Theory
Type
article
Field-Weighted Citation Impact
0.00

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article

Determination of the density of molecular flows falling on a body of arbitrary shape under conditions of free-molecular flow

Danil Korotkov
Bulletin of Federal State University of Education Series Physics and Mathematics
Gas Dynamics and Kinetic Theory
article

Determination of the density of molecular flows falling on a body of arbitrary shape under conditions of free-molecular flow

Danil Korotkov
article en

Abstract

Aim. The aim of this work was to develop an algorithm for determining the density of incident mass, momentum and energy flows on a body of complex shape, flown around by a highly rarefied gas. Methodology. The work uses methods of the molecular-kinetic theory of gases, aimed at determining the macroscopic characteristics of a rarefied gas flow. The work is based on the numerical solution of integrals of the Maxwell distribution function. Results. An algorithm has been developed and tested on a model simulating a device (solar battery panel, antenna, etc.) installed on the surface of a spacecraft body. Research implications . The developed algorithm can be used in problems related to determining the distribution of mass, momentum and energy flow densities over the surface of objects flown around by a highly rarefied gas medium, and in problems related to determining the characteristics of a spacecraft's own external atmosphere.

Bulletin of Federal State University of Education Series Physics and Mathematics(3)
Moscow Aviation Institute (RU)
Ministry of Education and Science of the Russian Federation
Openalex Percentile: Top 52%
Gas Dynamics and Kinetic Theory
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