Simulation of the Propeller Disk Inside the Symmetrical Channel

We work with the system of equations describing non-stationary compressible turbulent fluid flow, and we focus on the numerical solution of these equations, and on the boundary conditions. The computational simulation of the propeller disk is a demanding and time-consuming task. Here the propeller...

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Main Authors: Kyncl Martin, Pelant Jaroslav
Format: Article
Language:English
Published: EDP Sciences 2014-03-01
Series:EPJ Web of Conferences
Online Access:http://dx.doi.org/10.1051/epjconf/20146702064
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spelling doaj-e27b63c26acd413f999292dceeb79cd32021-08-02T16:13:30ZengEDP SciencesEPJ Web of Conferences2100-014X2014-03-01670206410.1051/epjconf/20146702064epjconf_efm-13_02064Simulation of the Propeller Disk Inside the Symmetrical ChannelKyncl Martin0Pelant Jaroslav1Výzkumný a Zkušební Letecký Ústav, a.s., VZLÚVýzkumný a Zkušební Letecký Ústav, a.s., VZLÚ We work with the system of equations describing non-stationary compressible turbulent fluid flow, and we focus on the numerical solution of these equations, and on the boundary conditions. The computational simulation of the propeller disk is a demanding and time-consuming task. Here the propeller disk is represented by the distribution of the vector of velocities along its radius. The main purpose is to describe the special compatible conditions used to simulate the propeller disk on the both its sides. In order to construct these conditions we analyze the equations in the close vicinity of the boundary. We use the analysis of the exact solution of the Riemann problem in order to solve this local boundary problem. The one-side modification of this problem has to be complemented with some other conditions. At the back side of the propeller disk, it is advantageous to use total density and the total pressure distribution, coming from the known distribution of axial velocities on the disk and the total state values at the inlet, and extra added velocities of rotation. At the front side of the disk, it is preferable to use the distribution of the flowing mass, known from the state values computed on the back side of the disk. We analyze the solution of these particular problems. We show the computational results of the flow around such propeller disk, obtained with the own-developed code for the solution of the 3D axis-symmetrical compressible turbulent gas flow. http://dx.doi.org/10.1051/epjconf/20146702064
collection DOAJ
language English
format Article
sources DOAJ
author Kyncl Martin
Pelant Jaroslav
spellingShingle Kyncl Martin
Pelant Jaroslav
Simulation of the Propeller Disk Inside the Symmetrical Channel
EPJ Web of Conferences
author_facet Kyncl Martin
Pelant Jaroslav
author_sort Kyncl Martin
title Simulation of the Propeller Disk Inside the Symmetrical Channel
title_short Simulation of the Propeller Disk Inside the Symmetrical Channel
title_full Simulation of the Propeller Disk Inside the Symmetrical Channel
title_fullStr Simulation of the Propeller Disk Inside the Symmetrical Channel
title_full_unstemmed Simulation of the Propeller Disk Inside the Symmetrical Channel
title_sort simulation of the propeller disk inside the symmetrical channel
publisher EDP Sciences
series EPJ Web of Conferences
issn 2100-014X
publishDate 2014-03-01
description We work with the system of equations describing non-stationary compressible turbulent fluid flow, and we focus on the numerical solution of these equations, and on the boundary conditions. The computational simulation of the propeller disk is a demanding and time-consuming task. Here the propeller disk is represented by the distribution of the vector of velocities along its radius. The main purpose is to describe the special compatible conditions used to simulate the propeller disk on the both its sides. In order to construct these conditions we analyze the equations in the close vicinity of the boundary. We use the analysis of the exact solution of the Riemann problem in order to solve this local boundary problem. The one-side modification of this problem has to be complemented with some other conditions. At the back side of the propeller disk, it is advantageous to use total density and the total pressure distribution, coming from the known distribution of axial velocities on the disk and the total state values at the inlet, and extra added velocities of rotation. At the front side of the disk, it is preferable to use the distribution of the flowing mass, known from the state values computed on the back side of the disk. We analyze the solution of these particular problems. We show the computational results of the flow around such propeller disk, obtained with the own-developed code for the solution of the 3D axis-symmetrical compressible turbulent gas flow.
url http://dx.doi.org/10.1051/epjconf/20146702064
work_keys_str_mv AT kynclmartin simulationofthepropellerdiskinsidethesymmetricalchannel
AT pelantjaroslav simulationofthepropellerdiskinsidethesymmetricalchannel
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