Syed Mohamed Ali, Jaffar and Mokhtar, Mohammad Solehan (2011) Propeller blade stress analysis using CATIA. In: Advances in Aircraft Structures. IIUM Press, Kuala Lumpur, pp. 30-36. ISBN 978-967-418-148-2
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Abstract
A procedure for modeling and stress analysis of a propeller blade using CATIA software have been detailed. The blade has been modeled with its twist angle and the results for different material have been presented graphically.
Item Type: | Book Chapter |
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Uncontrolled Keywords: | Propeller, design, stress, modeling, CATIA |
Subjects: | T Technology > TA Engineering (General). Civil engineering (General) > TA630 Structural engineering (General) |
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button): | Kulliyyah of Engineering > Department of Mechatronics Engineering |
Depositing User: | Dr Mohamed Ali Jaffar Syed |
Date Deposited: | 17 Jul 2012 14:57 |
Last Modified: | 17 Jul 2012 14:58 |
URI: | http://irep.iium.edu.my/id/eprint/24916 |
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