193   Artículos

 
en línea
Alexander Hergt, Tobias Danninger, Joachim Klinner, Sebastian Grund, Manfred Beversdorff and Christian Werner-Spatz    
In this paper, an experimental and numerical investigation of the effect of leading-edge erosion in transonic blades was performed. The measurements were carried out on a linear blade cascade in the Transonic Cascade Wind Tunnel of DLR in Cologne at two ... ver más

 
en línea
Ting Shi and Xueyuan Peng    
Air compressors in hydrogen fuel cell vehicles play a crucial role in ensuring the stability of the cathode air system. However, they currently face challenges related to low efficiency and poor stability. To address these issues, the experimental setup ... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Lucilene Silva, Tomas Grönstedt, Carlos Xisto, Luiz Whitacker, Cleverson Bringhenti and Marcus Lejon    
The ratio between blade height and chord, named the aspect ratio (AR), plays an important role in compressor aerodynamic design. Once selected, it influences stage performance, blade losses and the stage stability margin. The choice of the design AR invo... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yunfeng Wu, Qingkuo Li, Hang Yuan, Ziliang Li, Shiji Zhou, Ge Han and Xingen Lu    
High-pressure ratio centrifugal compressors? diffusers face challenges from high-velocity, non-uniform flow at the impeller outlet, decreasing efficiency and stall margin. To address this, this paper presents a novel vaned diffuser passage design method ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Shiyan Lin, Ruiyu Li, Limin Gao and Ning Ge    
The accurate prediction of tip leakage flow is the premise for flow mechanism analysis and compressor performance optimization. The detached eddy simulation (DES) method, which compromises cost and accuracy, has excellent potential for a high Reynolds fl... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Peng Zhang, Rixin Cheng and Yonghong Li    
Bionic herringbone riblets are applied to relieve the flow near the blade endwall in a linear compressor cascade under the incidence angle of -4° to 6° at a Reynolds number of 382,000. The herringbone riblets are placed at the endwall upstream of the bla... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
David S. Pellicer and Emilio Larrodé    
This paper shows the development of a numerical analysis model, which enables the calculation of the cargo transport capacity of a vehicle that circulates through a vacuum tube at high speed, whose effectiveness in transport is analyzed. The simulated tr... ver más
Revista: Algorithms    Formato: Electrónico

 
en línea
Lingfeng Zhong, Rui Liu, Xiaodong Miao, Yufeng Chen, Songhong Li and Haocheng Ji    
Compressors are important components in various power systems in the field of energy and power. In practical applications, compressors often operate under non-design conditions. Therefore, accurate calculation on performance under various operating condi... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Haoguang Zhang, Hao Wang, Qi Li, Fengyu Jing and Wuli Chu    
The aim of this research was to explore the mechanisms underlying the effect of self-circulating casing treatment with different circumferential coverage ratios on the aerodynamic performance of a transonic centrifugal compressor. A three-dimensional uns... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yang Zhao, Donghai Jin and Xingmin Gui    
Inlet distortion detrimentally affects the aerodynamic performance and lessens the stability of compressors, and has received considerable attention. The need to accurately estimate its effect on the performance and stability of compressor as early as po... ver más
Revista: Aerospace    Formato: Electrónico

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