16   Artículos

 
en línea
Seong Hyun Hong, Young Jin Kim, Soo Hyung Park, Sung Nam Jung and Ki Ro Kim    
The air and structural loads of a 5-ton class light helicopter (LH) rotor in a 2.24 g pull-up maneuver are investigated using a coupling between the computational structural dynamics (CSD) and computational fluid dynamics (CFD) methods. The LH rotor is c... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Pavol Kurdel, Natália Gecejová, Marek Ce?kovic and Anna Yakovlieva    
Unmanned aerial vehicle technology is the most advanced and helpful in almost every area of interest in human work. These devices become autonomous and can fulfil a variety of tasks, from simple imaging and obtaining data to search and rescue operations.... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Polina Talalaeva, Konstantin Starostin and Roman Savelyev    
In this article, a calculation model for a fuel system of a light helicopter was developed for experimental and operational testing. The model analyzes the operation of not only the units, but also the whole fuel system, offering the basis for functional... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Emanuele Luigi de Angelis, Fabrizio Giulietti, Gianluca Rossetti, Matteo Turci and Chiara Albertazzi    
Revista: Drones    Formato: Electrónico

 
en línea
Ruoyu Chen and Ying Chen    
To detect a desired underwater target quickly and precisely, a real-time sonar-based target detection system mounted on an autonomous underwater helicopter (AUH) using an improved convolutional neural network (CNN) is proposed in this paper. YOLOv5 is in... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
He Liu, Yu Dai, Jifu Jia and Xiang Zhu    
Lubricating oil flow characteristics are the primary concern in the main reducer of light helicopters. To improve the lubricating performance of the main reducer, a special lubrication system is innovatively constructed by adding two oil-guiding tubes to... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mei Yin, Xi Chen, Yu Dai, Duan Yang, Lanjin Xu and Xiang Zhu    
Limited by the space and weight of the reducer, it is difficult to use traditional oil-jet lubrication and splash lubrication for a light helicopter, so an oil-guiding splash lubrication method is adopted as a research object in this paper. Firstly, the ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Khiem Van Truong    
To fulfill the objective of a predictive tool for rotorcraft, comprehensive analysis (CA) needs to be capable of providing both accurate and time-efficient predictions of rotor air loads and structural loads. The more recent methodology based on comprehe... ver más
Revista: Aerospace    Formato: Electrónico

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