Propeller blade stress analysis using CATIA

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
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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