Aerodynamic design of annular ducts

This thesis presents mathematical and numerical methods for designing axisymmetric annular ducts having geometries capable of supporting fluid flows with prescribed performance characteristics. Three basic numerical methods of solution are given and are used to obtain results to the known exact solu...

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Main Author: Klier, A. M.
Format: Thesis
Language:English
Published: 1990
Subjects:
Online Access:https://repository.londonmet.ac.uk/3376/1/305115.pdf
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author Klier, A. M.
author_facet Klier, A. M.
author_sort Klier, A. M.
collection LMU
description This thesis presents mathematical and numerical methods for designing axisymmetric annular ducts having geometries capable of supporting fluid flows with prescribed performance characteristics. Three basic numerical methods of solution are given and are used to obtain results to the known exact solutions for a class of axisymmetric, irrotational incompressible flow regimes. Examination is made into the type of boundary conditions appropriate to control boundary layer behaviour and a new mixed boundary condition is derived to accomplish this. The technique is extended to cater for a class of swirling flows by investigating the derivation of a boundary layer approximation and further development allows the application of numerical iterative techniques to compressible flows with vorticity. These methods are especially suited to generating duct geometries with predetermined flow characteristics.
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spelling oai:repository.londonmet.ac.uk:33762018-09-26T10:58:04Z https://repository.londonmet.ac.uk/3376/ Aerodynamic design of annular ducts Klier, A. M. 530 Physics This thesis presents mathematical and numerical methods for designing axisymmetric annular ducts having geometries capable of supporting fluid flows with prescribed performance characteristics. Three basic numerical methods of solution are given and are used to obtain results to the known exact solutions for a class of axisymmetric, irrotational incompressible flow regimes. Examination is made into the type of boundary conditions appropriate to control boundary layer behaviour and a new mixed boundary condition is derived to accomplish this. The technique is extended to cater for a class of swirling flows by investigating the derivation of a boundary layer approximation and further development allows the application of numerical iterative techniques to compressible flows with vorticity. These methods are especially suited to generating duct geometries with predetermined flow characteristics. 1990-02 Thesis NonPeerReviewed text en https://repository.londonmet.ac.uk/3376/1/305115.pdf Klier, A. M. (1990) Aerodynamic design of annular ducts. Doctoral thesis, Polytechnic of North London.
spellingShingle 530 Physics
Klier, A. M.
Aerodynamic design of annular ducts
title Aerodynamic design of annular ducts
title_full Aerodynamic design of annular ducts
title_fullStr Aerodynamic design of annular ducts
title_full_unstemmed Aerodynamic design of annular ducts
title_short Aerodynamic design of annular ducts
title_sort aerodynamic design of annular ducts
topic 530 Physics
url https://repository.londonmet.ac.uk/3376/1/305115.pdf
work_keys_str_mv AT klieram aerodynamicdesignofannularducts