55   Artículos

 
en línea
Fangyou Yu, Zhanbiao Gao, Qifan Zhang, Lianjie Yue and Hao Chen    
Suppressing shock-induced flow separation has been a long-standing problem in the design of supersonic vehicles. To reduce the structural and design complexity of control devices, a passive control technique based on micro-serrations is proposed and its ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Aristia L. Philippou, Pavlos K. Zachos and David G. MacManus    
High-speed air intakes often exhibit intricate flow patterns, with a specific type of flow instability known as ?buzz?, characterized by unsteady shock oscillations at the inlet. This paper presents a comprehensive review of prior research, focused on un... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yiming Gong, Chuanqiang Gao and Weiwei Zhang    
The main buffet suppression techniques of aircrafts include active and passive flow control, aiming to reduce the impact of the fluctuating loads on the airfoil. These techniques are remedies after the airfoil design. The buffet suppression is not always... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Zhaoyong Mao, Tianqi Zhang, Guangyong Yang and Wenlong Tian    
Gurney flaps can enhance the hydrodynamic efficiency of airfoils, and they are currently used in several applications, including racing cars and wind turbines. However, there is a lack of studies in the literature on the application of Gurney flaps on th... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Davide Di Pasquale and Simon Prince    
Since modern transport aircraft cruise at transonic speeds, shock buffet alleviation is one indispensable challenge that civil transport research needs to be addressed. Indeed, in the transonic flow regime shock-induced separation and transonic buffet co... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mohammad Akhlaghi and Yahya Azizi    
In this paper, unsteady characteristics of a modified vaned-recessed casing treatment with 23.2% rotor blade tip axial chord exposure were studied numerically. The modifications to the traditional vaned-recessed casing treatments were composed of geometr... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yingzhe Zhang, Baohong Bai, Dakai Lin and Peiqing Liu    
The flap side-edge is a vital contributor to airframe noise. In this study, we propose a novel flap side-edge noise reduction method based on the concept of active blowing air. A long slot is opened from the flap?s lower surface to the tip surface to ind... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Ruixuan He, Xinjing Wang, Jian Li, Xiaodong Liu and Baowei Song    
Recently, inspired by the flippers of humpback whales, researchers have been widely studying leading-edge tubercles for use as passive flow control devices. In this research, we numerically investigated the effects of leading-edge tubercles on a three-di... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Zinnyrah Methal, Ahmad Syahin Abu Talib, Mohd Supian Abu Bakar, Mohd Rosdzimin Abdul Rahman, Mohamad Syafiq Sulaiman and Mohd Rashdan Saad    
This present study investigated the potential of passive flow control to reduce induced drag by using a micro-vortex generator (MVG) at a backward-facing step (BFS) location. A wing-in-ground (WIG) craft is a fast watercraft that resembles a dynamically ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Pengcheng Cui, Guiyu Zhou, Yaobing Zhang, Hongyin Jia, Xiaojun Wu, Mingsheng Ma, Huan Li and Bing Chen    
The internal weapon bay is widely used in modern aircraft; however, because the unsteady flows of the cavity would cause dangerous store separation and intense aerodynamic noise, the leading-edge spoiler is an easy and efficient passive flow-control meth... ver más
Revista: Aerospace    Formato: Electrónico

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