supported by the National Natural Science Foundation of China(Grant No.52076130)。
Supercritical carbon dioxide(SCO_(2))centrifugal compressor is a key component of a closed Brayton cycle system based on SCO_(2).A comprehensive understanding of the loss mechanism within the compressor is vital for i...
the National Natural Science Foundation of China for funding this work(Grant No.51676015).
The through-flow analysis is an important part in the compressor design process.In this part,lots of empirical models are used to predict the compressor aerodynamic performances.These models are all based on the early...
the National Key R&D Program of China(Grant No.2018YFB0106502);Open Fund of Science and Technology on Thermal Energy and Power Laboratory(No.TPL2017AB008).
Heightened interests have been laid at the preliminary design and optimization of the centrifugal compressor for the fuel cell vehicle.The centrifugal compressor for fuel cell vehicle is driven by a high-speed motor;h...
supported by the Long-Term Development Concept of Research Organization provided by the Ministry of Industry and Trade of the Czech Republic.
The kinetic energy loss and the secondary loss downstream of a high turning nozzle cascade were investigated.Influence of the incidence angle(i=-25°,0°and 25°)and Reynolds number(Re_(2,is)=0.8×10^(5),1.2×10^(5),...
support of the National Science Foundation of China(No.51406003);the National Science and Technology Major Project(J2019-II-0019-040)。
The effective control of the tip-leakage flow and loss is of great significance to improve the aerodynamic performance of the turbine.In this paper,the evolution mechanism of tip-leakage flow in a transonic high press...
supported by National Natural Science Foundation of China(No.51506152 and No.51777141);the Fundamental Research Funds for the Central Universities(inter-disciplinary program)under the contract No.kx0080020173427。
The regenerative refrigeration is an important reverse work-heat conversion cycle with a theoretical coefficient of performance(COP)identical to the Carnot efficiency.Practical regenerative refrigerators are capable o...
sponsored by the Project NO.51576037 supported by National Natural Science Foundation of China (NSFC)
This paper presents a numerical study on the aerodynamics loss reduction characteristics after the leading-edge(LE) optimization in a low-pressure turbine linear cascade. The LE was optimized with a simple and practic...
financial support from National Key R&D Program of China under Grant NO.2018YFB0606100;the National Natural Science Foundation of China under Grant NO. 51790510 and NO. 51727810
Casing treatments(CT) can effectively extend compressors flow ranges with the expense of efficiency penalty. Compressor efficiency is closely linked to loss. Only revealing the mechanisms of loss generation can design...
co-supported by the China Postdoctoral Science Foundation(Grant No.2017M621268);the National Natural Science Foundation of China(Grant Nos.51436002 and 51506020)
Curved blade and end-bend blade are considered as effective passive control methods for improving the aerodynamic performance of a compressor cascade,and their applicability also needs to be further studied.A highly-l...
the support from the National Natural Science Foundation of China (No.51679111, No.51409127 and No.51579118);Six Talents Peak Project of Jiangsu Province JNHB-CXTD-005;Natural Science Foundation of Jiangsu Province (BE2016163, BRA2017353 and No.BK20161472);Scientific research project of Jiangsu University(No.17A302);Priority Academic Program Development of Jiangsu Higher Education Institutions (PAPD) and National Key R&D Program Project (No.2017YFC0403703)
The conventional method cannot explicitly confirm the location and type of the energy loss, therefore this paper employs the entropy production theory to systematically analyze the category, magnitude and location of ...