Design and numerical simulation of the effect of heat transfer on the micro centrifugal compressor performance
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Design and numerical simulation of the effect of heat transfer on the micro centrifugal compressor performance
Vol. 25, Issue 4, (2010)
作者机构:
1. 中国科学院 研究生院,北京,100190
2. 中国科学院 工程热物理研究所,北京,100190
作者简介:
基金信息:
DOI:
CLC:
Published:2010
稿件说明:
移动端阅览
SHEN Yu-xin, LIU Jian-jun. Design and numerical simulation of the effect of heat transfer on the micro centrifugal compressor performance[J]. 2010, 25(4).
DOI:
SHEN Yu-xin, LIU Jian-jun. Design and numerical simulation of the effect of heat transfer on the micro centrifugal compressor performance[J]. 2010, 25(4).DOI:
Design and numerical simulation of the effect of heat transfer on the micro centrifugal compressor performance
A micro centrifugal compressor was designed for centimeter-scale micro turbomachinery
which has a diameter of 26 mm
designed rotate speed of 240 000 r/min
and designed mass flow rate of 30 g/s.Three-dimensional numerical simulations under adiabatic and isothermal conditions of solid wall were performed by using the commercial CFD(computational fluid dynamics) software CFX.The results show that
as compared with adiabatic condition
the mass flow rate at the isothermal condition decreases 7.53%
total to total isentropic efficiency decreases about 18.1%
total pressure rate decreases 21.7% at the same shaft work input.Taking the effect of heat transfer into account
the micro centrifugal-flow compressor was redesigned.CFX simulation results show that the improved design satisfies the design requirement of the micro turbomachinery.
Aerodynamic design method of high loaded supersonic axial-compressor with low reaction
Influences of several parameters on aerodynamic performance of micro-radial turbine
Aerodynamic design of highly-loaded blade in low-pressure turbine with low Reynolds number
Research on three-dimensional design of bowed and swept blade of transonic fan
Aerodynamic design and numerical simulation of a highly loaded transonic two-stage fan
Related Author
WANG Song-tao
HU Ying-jiao
WANG Zhong-qi
BIAN Lei
YAN Ze-Xiang
ZOU Zheng-ping
YANG Lin
QIAO Wei-yang
Related Institution
Engine Aerodynamic Research Center, School of Energy Science and Engineering, Harbin Institute of Technology
National Key Laboratory of of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion,Beijing University of Aeronautics and Astronautics
Department of System Engineering, China Aerospace Science and Technology Corporation
School of Power and Energy,Northwestern Polytechnical University
Gas Turbine Establishment, Aviation Industry Corporation of China