Material optimization of carbon/epoxy composite rotor for spacecraft energy storage
An investigation to optimize the carbon/epoxy composite rotor is performed for the spacecraft energy storage application. A high speed multi-layer rotor design is proposed and different composite materials are tested to achieve the most suitable recipe. First, the analytical rotor evaluation is perf...
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Multi Science Publishing
2010
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my.upm.eprints.155582015-10-08T00:52:51Z http://psasir.upm.edu.my/id/eprint/15558/ Material optimization of carbon/epoxy composite rotor for spacecraft energy storage Varatharajoo, Renuganth Salit, Mohd Sapuan Goh, Kian Hong An investigation to optimize the carbon/epoxy composite rotor is performed for the spacecraft energy storage application. A high speed multi-layer rotor design is proposed and different composite materials are tested to achieve the most suitable recipe. First, the analytical rotor evaluation is performed to establish a reliable numerical rotor model. Then, finite element analysis (FEA) is employed in order to optimise the multi-layer composite rotor design. Subsequently, the modal analysis is carried out to determine the rotor natural frequencies and mode shapes for a safe operational regime below 50, 000 rpm. Multi Science Publishing 2010 Article PeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/15558/1/Material%20optimization%20of%20carbon.pdf Varatharajoo, Renuganth and Salit, Mohd Sapuan and Goh, Kian Hong (2010) Material optimization of carbon/epoxy composite rotor for spacecraft energy storage. International Journal of Multiphysics, 4 (2). pp. 95-101. ISSN 1750-9548 10.1260/1750-9548.4.2.95 English |
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An investigation to optimize the carbon/epoxy composite rotor is performed for the spacecraft energy storage application. A high speed multi-layer rotor design is proposed and different composite materials are tested to achieve the most suitable recipe. First, the analytical rotor evaluation is performed to establish a reliable numerical rotor model. Then, finite element analysis (FEA) is employed in order to optimise the multi-layer composite rotor design. Subsequently, the modal analysis is carried out to determine the rotor natural frequencies and mode shapes for a safe operational regime below 50, 000 rpm. |
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Article |
author |
Varatharajoo, Renuganth Salit, Mohd Sapuan Goh, Kian Hong |
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Varatharajoo, Renuganth Salit, Mohd Sapuan Goh, Kian Hong Material optimization of carbon/epoxy composite rotor for spacecraft energy storage |
author_facet |
Varatharajoo, Renuganth Salit, Mohd Sapuan Goh, Kian Hong |
author_sort |
Varatharajoo, Renuganth |
title |
Material optimization of carbon/epoxy composite rotor for spacecraft energy storage |
title_short |
Material optimization of carbon/epoxy composite rotor for spacecraft energy storage |
title_full |
Material optimization of carbon/epoxy composite rotor for spacecraft energy storage |
title_fullStr |
Material optimization of carbon/epoxy composite rotor for spacecraft energy storage |
title_full_unstemmed |
Material optimization of carbon/epoxy composite rotor for spacecraft energy storage |
title_sort |
material optimization of carbon/epoxy composite rotor for spacecraft energy storage |
publisher |
Multi Science Publishing |
publishDate |
2010 |
url |
http://psasir.upm.edu.my/id/eprint/15558/1/Material%20optimization%20of%20carbon.pdf http://psasir.upm.edu.my/id/eprint/15558/ |
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