Structural design of a polymer matrix composite ship propeller

This work presents the structural design of a propeller, with its profile established using the OpenProp software for a 5 m long competition catamaran at a speed of 5.5 m/s. The materials selected using the Ashby method were polymer matrix composites, and the chosen manufacturing method was vacuum bagging. The determination of the stacking sequence was initially done using panel theory and the macromechanics of composite materials. The stacking sequence was then optimized using the finite element method with Abaqus CAE. Experimental validation was conducted through instrumented cantilever bending tests on both specimens and the blade. The finite element results showed errors of less than 5% compared to the experimental measurements, thus validating the simulations and allowing the blade to be designed with static safety factors greater than eight under operational service conditions.

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Publication Details

Journal
Advances in Mechanical Engineering
Published
2024-11-01
DOI
https://doi.org/10.1177/16878132241293616
Citations
1
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
1.30
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article

Structural design of a polymer matrix composite ship propeller

S. Jiménez, J. M. Meza, Julio Cuellar Posada
1 citations
Advances in Mechanical Engineering
Rocket and propulsion systems research
1.30
article

Structural design of a polymer matrix composite ship propeller

S. Jiménez, J. M. Meza, Julio Cuellar Posada
article en
1 citations

Abstract

This work presents the structural design of a propeller, with its profile established using the OpenProp software for a 5 m long competition catamaran at a speed of 5.5 m/s. The materials selected using the Ashby method were polymer matrix composites, and the chosen manufacturing method was vacuum bagging. The determination of the stacking sequence was initially done using panel theory and the macromechanics of composite materials. The stacking sequence was then optimized using the finite element method with Abaqus CAE. Experimental validation was conducted through instrumented cantilever bending tests on both specimens and the blade. The finite element results showed errors of less than 5% compared to the experimental measurements, thus validating the simulations and allowing the blade to be designed with static safety factors greater than eight under operational service conditions.

Advances in Mechanical EngineeringVol. 16(11)
Universidad Nacional de Colombia (CO)
Openalex Percentile: Top 12%
Rocket and propulsion systems research
1.30
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