Theoretical and experimental study of cycloidal propellers

Thesis (M.Eng.)--Memorial University of Newfoundland, 1991. Engineering and Applied Science Bibliography: leaves 93-97 Experiments were done on a model trochoidal propeller with a pitch ratio of 2.9247T in a cavitation tunnel in the Institute for Marine Dynamics (NRC). Problems which caused unreliab...

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Main Author: Li, Jin, 1960-
Other Authors: Memorial University of Newfoundland. Faculty of Engineering and Applied Science
Format: Thesis
Language:English
Published: 1991
Subjects:
Online Access:http://collections.mun.ca/cdm/ref/collection/theses3/id/32795
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spelling ftmemorialunivdc:oai:collections.mun.ca:theses3/32795 2023-05-15T17:23:32+02:00 Theoretical and experimental study of cycloidal propellers Li, Jin, 1960- Memorial University of Newfoundland. Faculty of Engineering and Applied Science 1991 xi, 276 leaves : ill. Image/jpeg; Application/pdf http://collections.mun.ca/cdm/ref/collection/theses3/id/32795 eng eng Electronic Theses and Dissertations (24.22 MB) -- http://collections.mun.ca/PDFs/theses/Li_Jin.pdf 76099308 http://collections.mun.ca/cdm/ref/collection/theses3/id/32795 The author retains copyright ownership and moral rights in this thesis. Neither the thesis nor substantial extracts from it may be printed or otherwise reproduced without the author's permission. Paper copy kept in the Centre for Newfoundland Studies, Memorial University Libraries Cycloidal propellers Text Electronic thesis or dissertation 1991 ftmemorialunivdc 2015-08-06T19:17:50Z Thesis (M.Eng.)--Memorial University of Newfoundland, 1991. Engineering and Applied Science Bibliography: leaves 93-97 Experiments were done on a model trochoidal propeller with a pitch ratio of 2.9247T in a cavitation tunnel in the Institute for Marine Dynamics (NRC). Problems which caused unreliable test results from a previous experimental study of the model propeller were examined. A mal-functioned torque transducer was replaced. Problems in the measurement of hydrodynamic torque and in calibration tests were analysed and effective ways to solve those problems were used in the present experimental study. Reliable test results for this model were obtained for propeller revolution speeds of 100,150,200 RPM. -- Mendenhall and Spangler's discrete vortex method of studying cycloidal propeller performance was modified so that (a) an angle of attack method was used to calculate effects of wake and other blades; (b) the modeling of dynamic stall effects were included; (c) three-dimensional effects of the blades were included. The theoretical results were compared with the experimental data from the present tests and from published results for cycloidal propellers with different pitch ratios and number of blade. It was found that the three dimensional correction method improved the predicted propeller performance at pitch ratios greater than 7r, The two dimensional model using the angle of attack method gave better prediction of propeller performance than other models at pitch ratios smaller than tt. The effectiveness of these models is discussed. Thesis Newfoundland studies University of Newfoundland Memorial University of Newfoundland: Digital Archives Initiative (DAI)
institution Open Polar
collection Memorial University of Newfoundland: Digital Archives Initiative (DAI)
op_collection_id ftmemorialunivdc
language English
topic Cycloidal propellers
spellingShingle Cycloidal propellers
Li, Jin, 1960-
Theoretical and experimental study of cycloidal propellers
topic_facet Cycloidal propellers
description Thesis (M.Eng.)--Memorial University of Newfoundland, 1991. Engineering and Applied Science Bibliography: leaves 93-97 Experiments were done on a model trochoidal propeller with a pitch ratio of 2.9247T in a cavitation tunnel in the Institute for Marine Dynamics (NRC). Problems which caused unreliable test results from a previous experimental study of the model propeller were examined. A mal-functioned torque transducer was replaced. Problems in the measurement of hydrodynamic torque and in calibration tests were analysed and effective ways to solve those problems were used in the present experimental study. Reliable test results for this model were obtained for propeller revolution speeds of 100,150,200 RPM. -- Mendenhall and Spangler's discrete vortex method of studying cycloidal propeller performance was modified so that (a) an angle of attack method was used to calculate effects of wake and other blades; (b) the modeling of dynamic stall effects were included; (c) three-dimensional effects of the blades were included. The theoretical results were compared with the experimental data from the present tests and from published results for cycloidal propellers with different pitch ratios and number of blade. It was found that the three dimensional correction method improved the predicted propeller performance at pitch ratios greater than 7r, The two dimensional model using the angle of attack method gave better prediction of propeller performance than other models at pitch ratios smaller than tt. The effectiveness of these models is discussed.
author2 Memorial University of Newfoundland. Faculty of Engineering and Applied Science
format Thesis
author Li, Jin, 1960-
author_facet Li, Jin, 1960-
author_sort Li, Jin, 1960-
title Theoretical and experimental study of cycloidal propellers
title_short Theoretical and experimental study of cycloidal propellers
title_full Theoretical and experimental study of cycloidal propellers
title_fullStr Theoretical and experimental study of cycloidal propellers
title_full_unstemmed Theoretical and experimental study of cycloidal propellers
title_sort theoretical and experimental study of cycloidal propellers
publishDate 1991
url http://collections.mun.ca/cdm/ref/collection/theses3/id/32795
genre Newfoundland studies
University of Newfoundland
genre_facet Newfoundland studies
University of Newfoundland
op_source Paper copy kept in the Centre for Newfoundland Studies, Memorial University Libraries
op_relation Electronic Theses and Dissertations
(24.22 MB) -- http://collections.mun.ca/PDFs/theses/Li_Jin.pdf
76099308
http://collections.mun.ca/cdm/ref/collection/theses3/id/32795
op_rights The author retains copyright ownership and moral rights in this thesis. Neither the thesis nor substantial extracts from it may be printed or otherwise reproduced without the author's permission.
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