50   Artículos

 
en línea
Valerie Hernley, Aleksandar Jemcov, Jeongseek Kang, Matthew Montgomery and Scott C. Morris    
The relationship between aerodynamic forcing and non-synchronous vibration (NSV) in axial compressors remains difficult to ascertain from experimental measurements. In this work, the relationship between casing pressure and blade vibration was investigat... ver más

 
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
Shiji Zhou, Shengfeng Zhao, Chuangxin Zhou, Yunfeng Wu, Hang Yuan and Xingen Lu    
To explore the internal flow mechanism and improve the performance of a supersonic compressor, an efficient global optimization design method was developed for an axial flow compressor and applied in the optimization design of a prototype supersonic comp... 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
Riccardo Toracchio, Fabrizio Fontaneto and Koen Hillewaert    
This paper presents the numerical characterization of a highly loaded compressor by means of 3D unsteady RANS simulations. The focus is on critical flow structures and their evolution at different operating points of the machine. First, the numerical set... ver más

 
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
Shenren Xu, Qian Zhang, Dingxi Wang and Xiuquan Huang    
Precise and inexpensive uncertainty quantification (UQ) is crucial for robust optimization of compressor blades and to control manufacturing tolerances. This study looks into the suitability of MC-adj-nonlinear, a nonlinear adjoint-based approach, to pre... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Shuai Ma, Jun Hu, Xuegao Wang and Jiajia Ji    
To make measurement of end-wall flow between blade rows in a compact multistage configuration possible, a miniature L-shaped five-hole probe was employed in this paper. This compact tip structure, realized by laser-printing instead of the conventional ma... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Xiaobin Xu, Ruoyu Wang, Xianjun Yu, Guangfeng An, Ying Qiu and Baojie Liu    
Three-dimensional blading is an efficient technique in compressor aerodynamic design, and its function mechanism in the cantilevered stator needs to be addressed. This paper focuses on the sweep and dihedral in the cantilevered stator and seeks to expose... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Shuli Hong, Jun Chi, Xin Xiang and Weiyu Lu    
A centrifugal compressor of a micro turbine generator system is investigated by the theoretical model and numerical analysis to explore the characteristics of the tip leakage vortex as the centrifugal compressor approaches stall. The numerical simulation... ver más
Revista: Aerospace    Formato: Electrónico

« Anterior     Página: 1 de 4     Siguiente »