ROTATING

作品数:789被引量:1076H指数:12
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相关作者:赖际舟刘建业张玲籍成宗赵科更多>>
相关机构:南京航空航天大学深圳大学清华大学北京航空航天大学更多>>
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Partial rotating instability in a boundary layer ingesting fan
《Chinese Journal of Aeronautics》2025年第3期43-64,共22页Hefang DENG Songan ZHANG Kailong XIA Xiaoqing QIANG Mingmin ZHU Jinfang TENG 
supports of the National Natural Science Foundation of China(Nos.52076129,92360308,52376027);the Shanghai Municipal Education Commission of China(No.2023-02-4);the Fundamental Research Funds for the Central Universities of China;the United Innovation Center(UIC)of Aerothermal Technologies for Turbomachinery of China.
Rotating Instability (RI) is a typical unsteady flow phenomenon in compressors and may cause severe aerodynamic noise and even potential nonsynchronous vibration. Most studies of RI are based on the uniform inflow, ig...
关键词:Rotating instability Boundary layer ingesting fan Tip leakage fAow Shear layer instability Full-annulus unsteady simnulation 
Vibration suppression for rotating space slender flexible structures based on novel deformation description and NNSMC controller with hyperbolic tangent function
《Chinese Journal of Aeronautics》2024年第10期339-364,共26页Dongyang SHANG Xiaopeng LI Men YIN Sainan ZHOU 
Supported by the Applied Basic Research Program of Liaoning Province,China(No.2023JH2/101300159);the National Natural Science Foundation of China(No.52275090).
Rotating Space Slender Flexible Structures(RSSFS)are extensively utilized in space operations because of their light weight,mobility,and low energy consumption.To realize the accurate space operation of the RSSFS,it i...
关键词:Space slender flexible structure Novel deformation description RBF neural network Vibration suppression Hyperbolic tangent function 
Experimental and computational investigation on flow characteristics of rotating cavities with high inlet pre-swirl axial throughflow被引量:1
《Chinese Journal of Aeronautics》2024年第4期276-293,共18页Sipeng WANG Xiang LUO Linji GUO Zeyu WU Yang BAI Zongchao LI Lichun MA 
As an integral part of the internal air system of aero-engines,the axial throughflow of the cooling air can interact with the cavity flow between the rotating compressor disks,forming a threedimensional,unsteady,and u...
关键词:Compressor Axial throughflow Rotating cavity flow Particle image velocimetry Unsteady RANS Flow pattern 
Investigation of anode shaping process during co-rotating electrochemical machining of convex structure on inner surface被引量:2
《Chinese Journal of Aeronautics》2023年第7期489-504,共16页Shuofang ZHOU Dengyong WANG Wenjian CAO Di ZHU 
supported by the National Natural Science Foundation of China(No.52175414);National Natural Science Foundation of China for Creative Research Groups(No.51921003);the China Postdoctoral Science Foundation(No.2019M661833).
A novel co-rotating electrochemical machining method is proposed for fabricating convex structures on the inner surface of a revolving part.The electrodes motion and material removal method of co-rotating electrochemi...
关键词:Convex structure forming process Co-rotating motion Current density Electrochemical machining Revolving part 
Experimental investigation of characteristics of instability evolution in a centrifugal compressor
《Chinese Journal of Aeronautics》2023年第4期174-189,共16页Hanzhi ZHANG Ce YANG Ben ZHAO Wei ZHAO Chenxing HU Wenli WANG Jianbing GAO Shijun SUN 
co-supported by the National Natural Science Foundation of China(Nos.51906006,51736001,52006217);the Beijing Institute of Technology Research Fund Program for Young Scholars,China.
The stable range of operation for the centrifugal compressor significantly influences the dynamic,economic,and environment-friendly characteristics of power systems.A deep understand-ing of the characteristics of inst...
关键词:Centrifugal compressor IMPELLERS Pressure measurement Rotating instability Stability STALL 
Leakage and wear characteristics of carbon seals for aero-engines被引量:3
《Chinese Journal of Aeronautics》2022年第11期389-400,共12页Guoqing LI Shen ZHANG Zhong KANG Yanfeng ZHANG Xingen LU Junqiang ZHU 
supported by the National Natural Science Foundation of China(No.51976214);National Science and Technology Major Project(2017-Ⅳ-0010-0047)。
Experimental investigation has been performed to study the leakage and wear characteristics of carbon seal working at high circumferential speed. To expand the scope of application, two newly designed carbon seals wer...
关键词:AERO-ENGINE Carbon seal Durability test LEAKAGE ROTATING Wear 
Electrochemical behavior of Ti-6.5Al-2Zr-1Mo-1V alloy under rotating condition with periodically fluctuating current density被引量:2
《Chinese Journal of Aeronautics》2022年第5期484-496,共13页Zhiyuan REN Dengyong WANG Juchen ZHANG Huayong LE Di ZHU 
funded by the National Natural Science Foundation of China(No.51805259);the National Natural Science Foundation of China for Creative Research Groups(No.51921003);the Natural Science Foundation of Jiangsu Province,China(Nos.BK20180431 and BK20190419);China Postdoctoral Science Foundation(Nos.2019M661833 and 2018M642246);Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology,China;the Young Elite Scientists Sponsorship Program by CAST,China。
Titanium alloy plays a crucial role in the electrochemical field due to its excellent corrosion resistance.The passivation and dissolution behaviors of Ti-6.5Al-2Zr-1Mo-1V(TA15)alloy in Na Cl solution were studied by ...
关键词:Dissolution Electrochemical behavior Passivation Rotating condition Ti-6.5Al-2Zr-1Mo-1V alloy 
Response and stabilization of a two-stage axial flow compressor restricted by rotating inlet distortion被引量:3
《Chinese Journal of Aeronautics》2021年第9期72-82,共11页Jia LI Xu DONG Dakun SUN Ruize XU Xiaofeng SUN 
supported by the National Natural Science Foundation of China(Nos.51822601,51790514 and 51906004)。
This paper considers effects of Rotating Inlet Distortion(RID)on a two-stage axial compressor and the stabilization effects of a casing treatment subjected to the considered RID.In multispool engines,the downstream co...
关键词:Axial compressors Casing treatment Inlet distortion Stall margin Stall precursor 
A review of recent studies on rotating internal cooling for gas turbine blades被引量:6
《Chinese Journal of Aeronautics》2021年第7期85-113,共29页Kirttayoth YERANEE Yu RAO 
The authors gratefully thank for the support of the National Science and Technology Major Project(No.2017-III-0009-0035);the National Natural Science Foundation of China(Nos.51676119 and 11972230).
Gas turbines have been used extensively for aircraft and marine propulsions as well as land-based power generation because of their high thermal efficiency and large power to weight ratios.To further increase the ther...
关键词:Flow characteristics Gas turbine blade Heat transfer Internal cooling ROTATION 
Instability characteristics of a co-rotating wingtip vortex pair based on bi-global linear stability analysis被引量:6
《Chinese Journal of Aeronautics》2021年第5期1-16,共16页Zepeng CHENG Siyi QIU Yang XIANG Chun SHAO Miao ZHANG Hong LIU 
co-supported by the National Basic Research Program of China(No.2014CB744802);Major Research of National Natural Science Foundation of China(No.91952302);China Postdoctoral Science Foundation(No.2018 M642007)。
The Stereo Particle Image Velocimetry(SPIV)technology is applied to measure the wingtip vortices generated by the up-down symmetrical split winglet.Then,the temporal biglobal Linear Stability Analysis(bi-global LSA)is...
关键词:Bi-global linear stability analysis Perturbation mode SPIV Vortex flow WINGLET Wingtip vortex 
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