TY - JOUR
T1 - Influence of inlet water ingestion on aero-engine fan-compressor performance
AU - Liu, Bo
AU - Cao, Zhi Peng
AU - Gao, Song
AU - Jin, Jun
AU - Zhou, Qiang
PY - 2005/12
Y1 - 2005/12
N2 - Numerical simulation and two-phase fluid flow theory were employed to calculate the characteristics of engine compressor with inlet water ingestion. Droplet model, loss and deviation model corrected by test data were used in the calculation. The investigation of water content, droplet size etc., which would affect the compressor performance, shows that inlet water content and size of droplets have significant influence on compressor performance. In addition the results indicate that this method is effective and valuable in engineering application.
AB - Numerical simulation and two-phase fluid flow theory were employed to calculate the characteristics of engine compressor with inlet water ingestion. Droplet model, loss and deviation model corrected by test data were used in the calculation. The investigation of water content, droplet size etc., which would affect the compressor performance, shows that inlet water content and size of droplets have significant influence on compressor performance. In addition the results indicate that this method is effective and valuable in engineering application.
KW - Aerospace propulsion system
KW - Compressor characteristics
KW - Droplet size
KW - Inlet water ingestion
KW - Loss and deviation model
UR - http://www.scopus.com/inward/record.url?scp=32844457967&partnerID=8YFLogxK
M3 - 文章
AN - SCOPUS:32844457967
SN - 1000-8055
VL - 20
SP - 1041
EP - 1047
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 6
ER -