Experimental and numerical investigation on solid propellant rocket motor performance

Application of Computational Fluid Dynamics (CFD) in studying solid propellant rocket motor have been growing steadily. This is due to the fact that experimental work will cost more time and money. Other than that, the industry needs more understanding to guide designer for more reliable technica...

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Main Author: Almayas, Ali A A A
Format: Thesis
Language:English
Published: 2021
Subjects:
Online Access:http://psasir.upm.edu.my/id/eprint/103996/1/ALI%20A%20A%20A%20ALMAYAS%20-%20IR.pdf
http://psasir.upm.edu.my/id/eprint/103996/
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spelling my.upm.eprints.1039962023-07-07T01:49:10Z http://psasir.upm.edu.my/id/eprint/103996/ Experimental and numerical investigation on solid propellant rocket motor performance Almayas, Ali A A A Application of Computational Fluid Dynamics (CFD) in studying solid propellant rocket motor have been growing steadily. This is due to the fact that experimental work will cost more time and money. Other than that, the industry needs more understanding to guide designer for more reliable technical solution and less expensive in order to design solid rocket motor for missiles and space launchers. To bring new knowledge for solid rocket propulsion, CFD has been important and dependable. However, to validate the dedicated models and numerical simulation, experimental procedure was important. For the design process, solid propellant rocket with medium thrust produced been focused in the current work. The works are including experimental and CFD simulation approaches. For the experimental work, the static firing test will be used. As for the fabrication of the propellant grain, it been conducted at the authorized centre by the Malaysian authority. Meanwhile for the CFD simulation, the work will be focus on the internal flow inside the nozzle. The findings show that data has significant errors due to the failure of the SRM bulkhead during experimental analysis. Due to the Covid 19 pandemic, the experimental work cannot be repeated and therefore was presented as it was. Next findings show the normal nozzle with different throat length simulation. It was found that the throat length has significant impact on the performance of the nozzle flow. Finally, findings from parametric study about the dual bell nozzle. The results show that the dual bell nozzle can increase the effectiveness of the nozzle flow. In overall, the work has covered all the intended objectives and CFD analysis has been prove as useful design tools used to lessen the amount of physical testing that must be done to validate a design and measure its performance. 2021-08 Thesis NonPeerReviewed text en http://psasir.upm.edu.my/id/eprint/103996/1/ALI%20A%20A%20A%20ALMAYAS%20-%20IR.pdf Almayas, Ali A A A (2021) Experimental and numerical investigation on solid propellant rocket motor performance. Doctoral thesis, Universiti Putra Malaysia. Solid propellants Computational fluid dynamics
institution Universiti Putra Malaysia
building UPM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Putra Malaysia
content_source UPM Institutional Repository
url_provider http://psasir.upm.edu.my/
language English
topic Solid propellants
Computational fluid dynamics
spellingShingle Solid propellants
Computational fluid dynamics
Almayas, Ali A A A
Experimental and numerical investigation on solid propellant rocket motor performance
description Application of Computational Fluid Dynamics (CFD) in studying solid propellant rocket motor have been growing steadily. This is due to the fact that experimental work will cost more time and money. Other than that, the industry needs more understanding to guide designer for more reliable technical solution and less expensive in order to design solid rocket motor for missiles and space launchers. To bring new knowledge for solid rocket propulsion, CFD has been important and dependable. However, to validate the dedicated models and numerical simulation, experimental procedure was important. For the design process, solid propellant rocket with medium thrust produced been focused in the current work. The works are including experimental and CFD simulation approaches. For the experimental work, the static firing test will be used. As for the fabrication of the propellant grain, it been conducted at the authorized centre by the Malaysian authority. Meanwhile for the CFD simulation, the work will be focus on the internal flow inside the nozzle. The findings show that data has significant errors due to the failure of the SRM bulkhead during experimental analysis. Due to the Covid 19 pandemic, the experimental work cannot be repeated and therefore was presented as it was. Next findings show the normal nozzle with different throat length simulation. It was found that the throat length has significant impact on the performance of the nozzle flow. Finally, findings from parametric study about the dual bell nozzle. The results show that the dual bell nozzle can increase the effectiveness of the nozzle flow. In overall, the work has covered all the intended objectives and CFD analysis has been prove as useful design tools used to lessen the amount of physical testing that must be done to validate a design and measure its performance.
format Thesis
author Almayas, Ali A A A
author_facet Almayas, Ali A A A
author_sort Almayas, Ali A A A
title Experimental and numerical investigation on solid propellant rocket motor performance
title_short Experimental and numerical investigation on solid propellant rocket motor performance
title_full Experimental and numerical investigation on solid propellant rocket motor performance
title_fullStr Experimental and numerical investigation on solid propellant rocket motor performance
title_full_unstemmed Experimental and numerical investigation on solid propellant rocket motor performance
title_sort experimental and numerical investigation on solid propellant rocket motor performance
publishDate 2021
url http://psasir.upm.edu.my/id/eprint/103996/1/ALI%20A%20A%20A%20ALMAYAS%20-%20IR.pdf
http://psasir.upm.edu.my/id/eprint/103996/
_version_ 1772813441049821184
score 13.159267