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Development of a perturbation potential panel method for analysing rotating 3D bodies

Thesis (MEng) -- University of Stellenbosch, 1996.

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Main Author: Furstenberg, Ludwig
Other Authors: Thiart, G. D.
Format: Thesis
Language:English
Published: Stellenbosch : Stellenbosch University 2012
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access_status_str Open Access
author Furstenberg, Ludwig
author2 Thiart, G. D.
author_browse Furstenberg, Ludwig
Thiart, G. D.
author_facet Thiart, G. D.
Furstenberg, Ludwig
author_sort Furstenberg, Ludwig
collection Thesis
dc_rights_str_mv Stellenbosch University
description Thesis (MEng) -- University of Stellenbosch, 1996.
format Thesis
id oai:scholar.sun.ac.za:10019.1/55046
institution Stellenbosch University (South Africa)
language English
last_indexed 2026-06-10T12:42:46.825Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository
publishDate 2012
publishDateRange 2012
publishDateSort 2012
publisher Stellenbosch : Stellenbosch University
publisherStr Stellenbosch : Stellenbosch University
record_format dspace
source_str SUNScholar — Stellenbosch University Repository
spelling oai:scholar.sun.ac.za:10019.1/55046 Development of a perturbation potential panel method for analysing rotating 3D bodies Furstenberg, Ludwig Thiart, G. D. Stellenbosch University. Faculty of Engineering. Dept. of Mechanical and Mechatronic Engineering. Propellers -- Data processing Fans (Machinery) -- Data processing Dissertations -- Mechanical engineering Thesis (MEng) -- University of Stellenbosch, 1996. The objective of this thesis was to develop a program to analyse steady, incompressible flow through a ducted propeller or fan. An extensive literature survey directed the project towards a perturbation potential based boundary element (panel) method. The work of Lee was instrumental to the construction of the present method. A modified Morino Kutta condition was implemented, rather than the non-linear pressure Kutta condition as proposed by Lee which necessitates extensive iterations. Three FORTRAN 77 programs were written to implement the method and various test cases are presented that verify the results produced by the program. Some problem areas are identified. Comparison between results predicted by the program and experimental results for local variation of pressure, as well as overall performance for an open propeller, demonstrates the practical value of the present method. A detailed analysis on a ducted fan system indicates a large increase in thrust produced when the blade loading is high. Although the maximum efficiency of the fan is slightly decreased when operating in a duct, an increase in efficiency is predicted at off-design conditions. Masters 2012-08-27T11:36:52Z 2012-08-27T11:36:52Z 1996 Thesis http://hdl.handle.net/10019.1/55046 en Stellenbosch University 132 pages : ill. application/pdf Stellenbosch : Stellenbosch University
spellingShingle Propellers -- Data processing
Fans (Machinery) -- Data processing
Dissertations -- Mechanical engineering
Furstenberg, Ludwig
Development of a perturbation potential panel method for analysing rotating 3D bodies
title Development of a perturbation potential panel method for analysing rotating 3D bodies
title_full Development of a perturbation potential panel method for analysing rotating 3D bodies
title_fullStr Development of a perturbation potential panel method for analysing rotating 3D bodies
title_full_unstemmed Development of a perturbation potential panel method for analysing rotating 3D bodies
title_short Development of a perturbation potential panel method for analysing rotating 3D bodies
title_sort development of a perturbation potential panel method for analysing rotating 3d bodies
topic Propellers -- Data processing
Fans (Machinery) -- Data processing
Dissertations -- Mechanical engineering
url http://hdl.handle.net/10019.1/55046
work_keys_str_mv AT furstenbergludwig developmentofaperturbationpotentialpanelmethodforanalysingrotating3dbodies