Stress And Aeroelastic Analyses Of Ultralight Aircraft Wing

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Stress And Aeroelastic Analyses Of Ultralight Aircraft Wing

This paper attempts to study a methodology stress analysis of an ultralight-aircraft’s wing structure imperiled to certain stress loads throughout the research. The analysis will cover static and flutter analysis of the wing’s structure. For static, it is more into lift distributions and the resulta...

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Bibliographic Details
Main Author:	Kabbarah, Hussam Fatthi A
Format:	Monograph
Language:	English
Published:	Universiti Sains Malaysia 2021
Subjects:	T Technology
Online Access:	http://eprints.usm.my/54530/ http://eprints.usm.my/54530/1/Stress%20And%20Aeroelastic%20Analyses%20Of%20Ultralight%20Aircraft%20Wing.pdf

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