TY - JOUR
T1 - Aerodynamic design of micro radial inflow turbine with wall heat transfer
AU - Ding, Chao
AU - Bian, Lei
AU - Zou, Zhengping
PY - 2014/7
Y1 - 2014/7
N2 - The heat transfer effect is a significant difference between the micro radial inflow turbine and the conventional radial inflow turbine, so it is very important to take the wall heat transfer effect into consideration when designing a micro radial inflow turbine. Based on the feature of non-adiabatic wall in the micro radial inflow turbine, and through theoretical analysis, a velocity diagram analytical model was obtained preliminarily. On that basis, the aerodynamic design method of the micro radial inflow turbine was developed. Then the design rule of the micro radial inflow turbine considering wall heat transfer effect was summarized. Finally a three-dimensional numerical simulation was carried out to verify the obtained model and design method. Results show that the model and design method of the micro radial inflow turbine considering wall heat transfer effect is feasible.
AB - The heat transfer effect is a significant difference between the micro radial inflow turbine and the conventional radial inflow turbine, so it is very important to take the wall heat transfer effect into consideration when designing a micro radial inflow turbine. Based on the feature of non-adiabatic wall in the micro radial inflow turbine, and through theoretical analysis, a velocity diagram analytical model was obtained preliminarily. On that basis, the aerodynamic design method of the micro radial inflow turbine was developed. Then the design rule of the micro radial inflow turbine considering wall heat transfer effect was summarized. Finally a three-dimensional numerical simulation was carried out to verify the obtained model and design method. Results show that the model and design method of the micro radial inflow turbine considering wall heat transfer effect is feasible.
KW - Design method
KW - Heat transfer effect
KW - Micro
KW - Numerical simulation
KW - Radial inflow turbine
UR - https://www.scopus.com/pages/publications/84905108614
U2 - 10.13700/j.bh.1001-5965.2013.0490
DO - 10.13700/j.bh.1001-5965.2013.0490
M3 - 文章
AN - SCOPUS:84905108614
SN - 1001-5965
VL - 40
SP - 947
EP - 952
JO - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
JF - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
IS - 7
ER -