A network approach for the prediction of flow and flow splits within a gas turbine combustor
The modern gas turbine engine industry needs a simpler and faster method to facilitate the design of gas turbine combustors due to the enormous costs of experimental test rigging and detailed computational fluid dynamics (CFD) simulations. Therefore, in the initial design phase, a couple of prelimin...
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Online Access: | http://hdl.handle.net/2263/26712 Pretorius, J 2005, A network approach for the prediction of flow and flow splits within a gas turbine combustor, MEng dissertation, University of Pretoria, Pretoria, viewed yymmdd < http://hdl.handle.net/2263/26712 > http://upetd.up.ac.za/thesis/available/etd-07272005-142518/ |
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ndltd-netd.ac.za-oai-union.ndltd.org-up-oai-repository.up.ac.za-2263-267122020-07-15T07:09:31Z A network approach for the prediction of flow and flow splits within a gas turbine combustor Pretorius, Johannes Jacobus Malan, A.G. Visser, J.A. pretoriusjohann@supremespring.co.za Flow splits Computational fluid dynamics Simple method Compressible and incompressible flow Variable area ducts Gas turbine combustors Gas dynamics Pipe network analysis UCTD The modern gas turbine engine industry needs a simpler and faster method to facilitate the design of gas turbine combustors due to the enormous costs of experimental test rigging and detailed computational fluid dynamics (CFD) simulations. Therefore, in the initial design phase, a couple of preliminary designs are conducted to establish initial values for combustor performance and geometric characteristics. In these preliminary designs, various one-dimensional models using analytical and empirical formulations may be used. One of the disadvantages of existing models is that they are typically geometric dependant, i.e. they apply only to the geometry they are derived for. Therefore the need for a more versatile design tool exists. In this work, which constitutes the first step in the development of such a versatile design tool, a single equation-set network simulation model to describe both steady state compressible and incompressible isothermal flow is developed. The continuity and momentum equations are solved through a hybrid type network model analogy which makes use of the SIMPLE pressure correction methodology. The code has the capability to efficiently compute flow through elements where the loss factor K is highly flow dependant and accurately describes variable area duct flow in the case of incompressible flow. The latter includes ducts with discontinuously varying flow sectional areas. Proper treatment of flow related non-linearities, such as flow friction, is facilitated in a natural manner in the proposed methodology. The proposed network method is implemented into a Windows based simulation package with a user interface. The ability of the proposed method to accurately model both compressible and incompressible flow is demonstrated through the analyses of a number of benchmark problems. It will be shown that the proposed methodology yields similar or improved results as compared to other’s work. The proposed method is applied to a research combustor to solve for isothermal flows and flow splits. The predicted flows were in relatively close agreement with measured data as well as detailed CFD analysis. Dissertation (MEng (Mechanical Engineering))--University of Pretoria, 2005. Mechanical and Aeronautical Engineering unrestricted 2013-09-07T07:18:24Z 2005-07-27 2013-09-07T07:18:24Z 2005-03-10 2005 2005-07-27 Dissertation http://hdl.handle.net/2263/26712 Pretorius, J 2005, A network approach for the prediction of flow and flow splits within a gas turbine combustor, MEng dissertation, University of Pretoria, Pretoria, viewed yymmdd < http://hdl.handle.net/2263/26712 > http://upetd.up.ac.za/thesis/available/etd-07272005-142518/ © 2005, University of Pretoria. All rights reserved. The copyright in this work vests in the University of Pretoria. No part of this work may be reproduced or transmitted in any form or by any means, without the prior written permission of the University of Pretoria. University of Pretoria |
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Flow splits Computational fluid dynamics Simple method Compressible and incompressible flow Variable area ducts Gas turbine combustors Gas dynamics Pipe network analysis UCTD |
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Flow splits Computational fluid dynamics Simple method Compressible and incompressible flow Variable area ducts Gas turbine combustors Gas dynamics Pipe network analysis UCTD Pretorius, Johannes Jacobus A network approach for the prediction of flow and flow splits within a gas turbine combustor |
description |
The modern gas turbine engine industry needs a simpler and faster method to facilitate the design of gas turbine combustors due to the enormous costs of experimental test rigging and detailed computational fluid dynamics (CFD) simulations. Therefore, in the initial design phase, a couple of preliminary designs are conducted to establish initial values for combustor performance and geometric characteristics. In these preliminary designs, various one-dimensional models using analytical and empirical formulations may be used. One of the disadvantages of existing models is that they are typically geometric dependant, i.e. they apply only to the geometry they are derived for. Therefore the need for a more versatile design tool exists. In this work, which constitutes the first step in the development of such a versatile design tool, a single equation-set network simulation model to describe both steady state compressible and incompressible isothermal flow is developed. The continuity and momentum equations are solved through a hybrid type network model analogy which makes use of the SIMPLE pressure correction methodology. The code has the capability to efficiently compute flow through elements where the loss factor K is highly flow dependant and accurately describes variable area duct flow in the case of incompressible flow. The latter includes ducts with discontinuously varying flow sectional areas. Proper treatment of flow related non-linearities, such as flow friction, is facilitated in a natural manner in the proposed methodology. The proposed network method is implemented into a Windows based simulation package with a user interface. The ability of the proposed method to accurately model both compressible and incompressible flow is demonstrated through the analyses of a number of benchmark problems. It will be shown that the proposed methodology yields similar or improved results as compared to other’s work. The proposed method is applied to a research combustor to solve for isothermal flows and flow splits. The predicted flows were in relatively close agreement with measured data as well as detailed CFD analysis. === Dissertation (MEng (Mechanical Engineering))--University of Pretoria, 2005. === Mechanical and Aeronautical Engineering === unrestricted |
author2 |
Malan, A.G. |
author_facet |
Malan, A.G. Pretorius, Johannes Jacobus |
author |
Pretorius, Johannes Jacobus |
author_sort |
Pretorius, Johannes Jacobus |
title |
A network approach for the prediction of flow and flow splits within a gas turbine combustor |
title_short |
A network approach for the prediction of flow and flow splits within a gas turbine combustor |
title_full |
A network approach for the prediction of flow and flow splits within a gas turbine combustor |
title_fullStr |
A network approach for the prediction of flow and flow splits within a gas turbine combustor |
title_full_unstemmed |
A network approach for the prediction of flow and flow splits within a gas turbine combustor |
title_sort |
network approach for the prediction of flow and flow splits within a gas turbine combustor |
publisher |
University of Pretoria |
publishDate |
2013 |
url |
http://hdl.handle.net/2263/26712 Pretorius, J 2005, A network approach for the prediction of flow and flow splits within a gas turbine combustor, MEng dissertation, University of Pretoria, Pretoria, viewed yymmdd < http://hdl.handle.net/2263/26712 > http://upetd.up.ac.za/thesis/available/etd-07272005-142518/ |
work_keys_str_mv |
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1719326143387009024 |