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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| Format: | Monograph |
| Language: | English |
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Universiti Sains Malaysia
2017
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| Online Access: | http://eprints.usm.my/51667/1/Determining%20Helicopter%20Blade%20Length%20Per%20Airworthiness%20Strength%20Requirement_Nur%20Ika%20Farhana%20Sariman_A2_2017.pdf |