Determining Helicopter Blade Length Per Airworthiness Strength Requirement

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Determining Helicopter Blade Length Per Airworthiness Strength Requirement

This paper demonstrates a methodology to determine the length of a metal helicopter rotor blade operating at 500 RPM so that it fulfills the airworthiness strength requirement. To achieve this, stress analyses were performed on different blade length using SOLIDWORKS 2016 x64 Edition. The NACA 8-H-1...

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Bibliographic Details
Main Author:	Sariman, Nur Ika Farhana
Format:	Monograph
Language:	English
Published:	Universiti Sains Malaysia 2017
Subjects:	T Technology
Online Access:	http://eprints.usm.my/51667/ http://eprints.usm.my/51667/1/Determining%20Helicopter%20Blade%20Length%20Per%20Airworthiness%20Strength%20Requirement_Nur%20Ika%20Farhana%20Sariman_A2_2017.pdf

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