Title: Thrust response experiments of a variable pitch propeller rotor
Abstract: In the design and development of UAV (unmanned aerial vehicle), application of a variable pitch propeller which can freely change the propeller angle is expected. In this presentation, we report the frequency response of thrust change with propeller pitch angle input.
Publication Year: 2017
Publication Date: 2017-01-01
Language: en
Type: article
Indexed In: ['crossref']
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