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Development of educational software for stress analysis of an aircraft wing
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نویسنده
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mohamed ali j.s. ,sadeq t.
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منبع
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journal of engineering science and technology - 2012 - دوره : 7 - شماره : 3 - صفحه:322 -338
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چکیده
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A stress analysis software based on matlab,graphic user interface (gui) has been developed. the developed software can be used to estimate load on a wing and to compute the stresses at any point along the span of the wing of a given aircraft. the generalized formulation allows performing stress analysis even for a multispar (multicell) wing. the software is expected to be a useful tool for effective teaching learning process of courses on aircraft structures and aircraft structural design. © school of engineering,taylor's university.
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کلیدواژه
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Aircraft wings; Education; Matlab; Software; Stress analysis
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آدرس
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department of mechanical engineering,kulliyah of engineering,international islamic university malaysia (iium),p.o. box no. 10,50728, Malaysia, department of mechanical engineering,kulliyah of engineering,international islamic university malaysia (iium),p.o. box no. 10,50728, Malaysia
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Authors
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