A Discontinuous Galerkin–Finite Element Method for the Nonlinear Unsteady Burning Rate Responses of Solid Propellants

The unsteady combustion of solid propellants under oscillating environments is the key to understanding the combustion instability inside solid rocket motors. The discontinuous Galerkin–finite element method (DG-FEM) is introduced to provide an efficient yet flexible numerical platform to investigat...

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Main Authors: Zhuopu Wang, Kairui Yu, Yuanzhe Liu
Format: Article
Language:English
Published: MDPI AG 2024-01-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/11/1/97
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author Zhuopu Wang
Kairui Yu
Yuanzhe Liu
author_facet Zhuopu Wang
Kairui Yu
Yuanzhe Liu
author_sort Zhuopu Wang
collection DOAJ
description The unsteady combustion of solid propellants under oscillating environments is the key to understanding the combustion instability inside solid rocket motors. The discontinuous Galerkin–finite element method (DG-FEM) is introduced to provide an efficient yet flexible numerical platform to investigate the combustion dynamics of solid propellants. The algorithm is developed for the classical unsteady model, the Zel’dovich–Novozhilov model. It is then validated based on a special analytical solution. The DG-FEM algorithm is then compared with the classical spectral method based on Laguerre polynomials. It is shown that the DG-FEM works more efficiently than the traditional spectral method, providing a more accurate solution with a lower computational cost.
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spelling doaj.art-d07e5a554c374df99c6e22ff037819fc2024-01-26T14:14:23ZengMDPI AGAerospace2226-43102024-01-011119710.3390/aerospace11010097A Discontinuous Galerkin–Finite Element Method for the Nonlinear Unsteady Burning Rate Responses of Solid PropellantsZhuopu Wang0Kairui Yu1Yuanzhe Liu2National Key Laboratory of Solid Rocket Propulsion, Northwestern Polytechnical University, Xi’an 710072, ChinaNational Key Laboratory of Solid Rocket Propulsion, Northwestern Polytechnical University, Xi’an 710072, ChinaNational Key Laboratory of Solid Rocket Propulsion, Northwestern Polytechnical University, Xi’an 710072, ChinaThe unsteady combustion of solid propellants under oscillating environments is the key to understanding the combustion instability inside solid rocket motors. The discontinuous Galerkin–finite element method (DG-FEM) is introduced to provide an efficient yet flexible numerical platform to investigate the combustion dynamics of solid propellants. The algorithm is developed for the classical unsteady model, the Zel’dovich–Novozhilov model. It is then validated based on a special analytical solution. The DG-FEM algorithm is then compared with the classical spectral method based on Laguerre polynomials. It is shown that the DG-FEM works more efficiently than the traditional spectral method, providing a more accurate solution with a lower computational cost.https://www.mdpi.com/2226-4310/11/1/97discontinuous Galerkinnumerical algorithmsolid propellantunsteady responsecombustion instability
spellingShingle Zhuopu Wang
Kairui Yu
Yuanzhe Liu
A Discontinuous Galerkin–Finite Element Method for the Nonlinear Unsteady Burning Rate Responses of Solid Propellants
Aerospace
discontinuous Galerkin
numerical algorithm
solid propellant
unsteady response
combustion instability
title A Discontinuous Galerkin–Finite Element Method for the Nonlinear Unsteady Burning Rate Responses of Solid Propellants
title_full A Discontinuous Galerkin–Finite Element Method for the Nonlinear Unsteady Burning Rate Responses of Solid Propellants
title_fullStr A Discontinuous Galerkin–Finite Element Method for the Nonlinear Unsteady Burning Rate Responses of Solid Propellants
title_full_unstemmed A Discontinuous Galerkin–Finite Element Method for the Nonlinear Unsteady Burning Rate Responses of Solid Propellants
title_short A Discontinuous Galerkin–Finite Element Method for the Nonlinear Unsteady Burning Rate Responses of Solid Propellants
title_sort discontinuous galerkin finite element method for the nonlinear unsteady burning rate responses of solid propellants
topic discontinuous Galerkin
numerical algorithm
solid propellant
unsteady response
combustion instability
url https://www.mdpi.com/2226-4310/11/1/97
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