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Internal ballistic modelling of solid rocket motors using level set methods for simulating grain burnback

Thesis (MSc)--Stellenbosch University, 2016

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Main Author: Tshokotsha, Mvuyisi Humprey
Other Authors: Maritz, Milton Frick
Format: Thesis
Language:en_ZA
Published: Stellenbosch : Stellenbosch University 2016
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access_status_str Open Access
author Tshokotsha, Mvuyisi Humprey
author2 Maritz, Milton Frick
author_browse Maritz, Milton Frick
Tshokotsha, Mvuyisi Humprey
author_facet Maritz, Milton Frick
Tshokotsha, Mvuyisi Humprey
author_sort Tshokotsha, Mvuyisi Humprey
collection Thesis
dc_rights_str_mv Stellenbosch University
description Thesis (MSc)--Stellenbosch University, 2016
format Thesis
id oai:scholar.sun.ac.za:10019.1/98839
institution Stellenbosch University (South Africa)
language en_ZA
last_indexed 2026-06-10T12:44:22.712Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository
publishDate 2016
publishDateRange 2016
publishDateSort 2016
publisher Stellenbosch : Stellenbosch University
publisherStr Stellenbosch : Stellenbosch University
record_format dspace
source_str SUNScholar — Stellenbosch University Repository
spelling oai:scholar.sun.ac.za:10019.1/98839 Internal ballistic modelling of solid rocket motors using level set methods for simulating grain burnback Tshokotsha, Mvuyisi Humprey Maritz, Milton Frick Stellenbosch University. Faculty of Science. Department Mathematical Science. Applied Mathematics Level set methods Solid rocket motors Grain burnback analysis Rockets -- Models Rockets -- Simulation Thesis (MSc)--Stellenbosch University, 2016 ENGLISH ABSTRACT : Solid Rocket Motors are propulsive systems providing thrust from products exiting through a nozzle, obtained by burning a solid fuel (the grain) inside a chamber. Various thrust profiles can be obtained by different initial grain geometries. The purpose of numerical modelling, is to predict the thrust curve, given an initial geometry. A simplified model for Solid Rocket Motor behaviour is developed. The grain geometry is represented by a signed distance function, and the burning surface geometry is calculated using a numerical solution of the burning process based on level-set methods. The gas flux is modelled using a 1-D approximation of the gas dynamics inside the chamber, following a method proposed by Lamberty. 2D and 3D models for modelling the regression of the grain surface over time are developed. The evolution of different grain geometries are simulated and the results obtained are compared to the experimental data available. The burning surface and port area for some grain geometries is calculated analytically and the results found are compared with the ones found numerically using 2D model of the level set method. AFRIKAANSE OPSOMMING : Vastevuurpylmotore is ’n aandrywingstelsel wat stukrag verskaf vanaf gas wat by ’n spuitstuk uitspuit, waar die gas van die verbranding van ‘n vaste brandstof (genoem die grein) in ’n ontbrandingskamer afkomstig is. Verskeie stukrag krommes kan deur verskillende aanvanklike grein geometrie´’e verkry word. Die doel van numeriese modellering is om die stukrag kromme te voorspel uit die aanvanklike grein-geometrie. ’n Vereenvoudigde model vir Vastevuurpylmotorgedrag word ontwikkel. Die grein geometrie word deur ’n tekenafhanklike afstandsfunksie voorgestel en die brandoppervlak word deur numeriese oplossing van die brandproses, gebasseer op kontoervlak-metodes, bereken. Die gasvloei word met ’n 1D benadering van die gasdinamika binne die ontbrandingskamer gemodelleer, geskoei op ’n metode voorgestel deur Lamberty. 2D en 3D modelle vir die tydsafhanklike wegbrand van die greinoppervlak word ontwikkel. Die evolusie van verskillende grein geometrie´’e word gesimuleer en die resultate word met beskikbare eksperimentele data vergelyk. Die area van die brandoppervlak, sowel as die kanaalvloeiarea word analities bereken vir ’n aantal grein-geometrie´’e en dit word vergelyk met die ooreenstemmende areas soos numeries bereken deur die 2D model van die kontoervlak-metode. 2016-03-09T15:08:11Z 2016-03-09T15:08:11Z 2016-03 Thesis http://hdl.handle.net/10019.1/98839 en_ZA Stellenbosch University xviii, 106 pages : illustrations (some colour) application/pdf Stellenbosch : Stellenbosch University
spellingShingle Level set methods
Solid rocket motors
Grain burnback analysis
Rockets -- Models
Rockets -- Simulation
Tshokotsha, Mvuyisi Humprey
Internal ballistic modelling of solid rocket motors using level set methods for simulating grain burnback
title Internal ballistic modelling of solid rocket motors using level set methods for simulating grain burnback
title_full Internal ballistic modelling of solid rocket motors using level set methods for simulating grain burnback
title_fullStr Internal ballistic modelling of solid rocket motors using level set methods for simulating grain burnback
title_full_unstemmed Internal ballistic modelling of solid rocket motors using level set methods for simulating grain burnback
title_short Internal ballistic modelling of solid rocket motors using level set methods for simulating grain burnback
title_sort internal ballistic modelling of solid rocket motors using level set methods for simulating grain burnback
topic Level set methods
Solid rocket motors
Grain burnback analysis
Rockets -- Models
Rockets -- Simulation
url http://hdl.handle.net/10019.1/98839
work_keys_str_mv AT tshokotshamvuyisihumprey internalballisticmodellingofsolidrocketmotorsusinglevelsetmethodsforsimulatinggrainburnback