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Study of a flexible UAV proprotor

Mohd Zawawi, Fazila and Lv, Peng and Prothin, Sebastien and Morlier, Joseph and Moschetta, Jean-Marc and Bénard, Emmanuel Study of a flexible UAV proprotor. (2014) International Journal of Engineering Systems Modelling and Simulation, 6 (3/4). 149-161. ISSN 1755-9758

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Abstract

This paper is concerned with the evaluation of design techniques, both for the propulsive performance and for the structural behaviour of a composite flexible proprotor. A numerical model was developed using a combination of aerodynamic model based on blade element momentum theory (BEMT), and structural model based on anisotropic beam finite element, in order to evaluate the coupled structural and the aerodynamic characteristics of the deformable proprotor blade. The numerical model was then validated by means of static performance measurements and shape reconstruction from laser distance sensor outputs. From the validation results of both aerodynamic and structural model, it can be concluded that the numerical approach developed by the authors is valid as a reliable tool for designing and analysing the UAV-sized proprotor made of composite material. The proposed experiment technique is also capable of providing a predictive and reliable data in blade geometry and performance for rotor modes.

Item Type:Article
HAL Id:hal-01851591
Audience (journal):International peer-reviewed journal
Uncontrolled Keywords:
Institution:Université de Toulouse > Ecole nationale supérieure des Mines d'Albi-Carmaux - IMT Mines Albi (FRANCE)
Université de Toulouse > Institut National des Sciences Appliquées de Toulouse - INSA (FRANCE)
Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE)
Université de Toulouse > Université Toulouse III - Paul Sabatier - UPS (FRANCE)
Laboratory name:
Funders:
Malaysian Ministry of Higher Education - China Scholarship Council
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Deposited By: Fazila Mohd Zawawi
Deposited On:03 Apr 2014 09:57

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