A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems

Inlet as part of aircraft engine plays important role in controlling the rate of airflow entering to the engine. The shape of inlet has to be designed in such away to make the rate of airflow does not change too much with angle of attack and also not much pressure losses at the time, the airflow ent...

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Bibliographic Details
Main Author:	Altaher Mohamed , Mohamed Abdalwahab
Format:	Thesis
Published:	2011
Subjects:	TL500-778 Aeronautics. Aeronautical engineering
Online Access:	http://eprints.uthm.edu.my/1737/ http://eprints.uthm.edu.my/1737/1/MOHAMED_ABDALWAHAB_ALTAHER_MOHAMED.pdf

id	uthm-1737
recordtype	eprints
spelling	uthm-17372011-08-19T08:02:41Z A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems Altaher Mohamed , Mohamed Abdalwahab TL500-778 Aeronautics. Aeronautical engineering Inlet as part of aircraft engine plays important role in controlling the rate of airflow entering to the engine. The shape of inlet has to be designed in such away to make the rate of airflow does not change too much with angle of attack and also not much pressure losses at the time, the airflow entering to the compressor section. It is therefore understanding on the flow pattern inside the inlet is important. The present work presents on the use of the Fourth Order Runge Kutta – Harten Yee TVD scheme [1, 2] for the flow analysis inside inlet. The flow is assumed as an inviscid quasi two dimensional compressible flow. As an initial stage of computer code development, here uses three generic inlet models. The first inlet model to allow the problem in hand solved as the case of inlet with expansion wave case. The second inlet model will relate to the case of expansion compression wave. The last inlet model concerns with the inlet which produce series of weak shock wave and end up with a normal shock wave. The comparison result for the same test case with Fluent Software [3] indicates that the developed computer code based on the Fourth Order Runge Kutta – Harten – Yee TVD scheme are very close to each other. However for complex inlet geometry, the problem is in the way how to provide an appropriate mesh model. 2011-01 Thesis NonPeerReviewed application/pdf http://eprints.uthm.edu.my/1737/1/MOHAMED_ABDALWAHAB_ALTAHER_MOHAMED.pdf Altaher Mohamed , Mohamed Abdalwahab (2011) A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems. Masters thesis, Universiti Tun Hussein Onn Malaysia. http://eprints.uthm.edu.my/1737/
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Tun Hussein Onn Malaysia
building	UTHM Institutional Repository
collection	Online Access
topic	TL500-778 Aeronautics. Aeronautical engineering
spellingShingle	TL500-778 Aeronautics. Aeronautical engineering Altaher Mohamed , Mohamed Abdalwahab A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems
description	Inlet as part of aircraft engine plays important role in controlling the rate of airflow entering to the engine. The shape of inlet has to be designed in such away to make the rate of airflow does not change too much with angle of attack and also not much pressure losses at the time, the airflow entering to the compressor section. It is therefore understanding on the flow pattern inside the inlet is important. The present work presents on the use of the Fourth Order Runge Kutta – Harten Yee TVD scheme [1, 2] for the flow analysis inside inlet. The flow is assumed as an inviscid quasi two dimensional compressible flow. As an initial stage of computer code development, here uses three generic inlet models. The first inlet model to allow the problem in hand solved as the case of inlet with expansion wave case. The second inlet model will relate to the case of expansion compression wave. The last inlet model concerns with the inlet which produce series of weak shock wave and end up with a normal shock wave. The comparison result for the same test case with Fluent Software [3] indicates that the developed computer code based on the Fourth Order Runge Kutta – Harten – Yee TVD scheme are very close to each other. However for complex inlet geometry, the problem is in the way how to provide an appropriate mesh model.
format	Thesis
author	Altaher Mohamed , Mohamed Abdalwahab
author_facet	Altaher Mohamed , Mohamed Abdalwahab
author_sort	Altaher Mohamed , Mohamed Abdalwahab
title	A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems
title_short	A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems
title_full	A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems
title_fullStr	A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems
title_full_unstemmed	A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems
title_sort	comparative study fourth order runge kutta-tvd scheme and fluent software case of inlet flow problems
publishDate	2011
url	http://eprints.uthm.edu.my/1737/ http://eprints.uthm.edu.my/1737/1/MOHAMED_ABDALWAHAB_ALTAHER_MOHAMED.pdf
first_indexed	2018-09-05T10:52:32Z
last_indexed	2018-09-05T10:52:32Z
_version_	1610764520069791744

A comparative study fourth order runge KUTTA-TVD scheme and fluent software case of inlet flow problems

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