Stress And Strength Analyses Of Ultra-Light Aircraft Fuselage

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Stress And Strength Analyses Of Ultra-Light Aircraft Fuselage

Ultra-light aircraft is a special kind of low-speed general aircraft. It is low weighted and small-sized however can depart and land without changing the structure of any parts. This thesis is the case study on the stress and strength analyses of an ultra-light aircraft fuselage about its performanc...

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Bibliographic Details
Main Author:	Saironi, Muhammad Isa
Format:	Monograph
Language:	English
Published:	Universiti Sains Malaysia 2021
Subjects:	T Technology
Online Access:	http://eprints.usm.my/54624/ http://eprints.usm.my/54624/1/Stress%20And%20Strength%20Analyses%20Of%20Ultra-Light%20Aircraft%20Fuselage.pdf

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