TY - GEN
T1 - Incipient rotating stall characteristics measured by semiconductor L2F and pressure transducer in vaneless diffusers of centrifugal blowers
AU - Ishida, Masahiro
AU - Sakaguchi, Daisaku
AU - Ueki, Hironobu
N1 - Publisher Copyright:
© Copyright 2000 by ASME.
PY - 2000
Y1 - 2000
N2 - In order to clarify the transient behavior from the non-stall condition to the developed rotating stall in vaneless diffuser of a centrifugal blower, blade-to-blade variations of velocity and wall pressure were measured immediately upstream and downstream of the impeller exit as well as in the vaneless diffuser by means of the semiconductor laser 2-focus velocimeter and the pressure sensor respectively. The specified auto-correlation coefficient of large scale disturbances with the wavelength larger than twice of the blade spacing show that the intermittent stall occurs prior to the developed rotating stall. By analyzing the flow-fluctuationellipse and the correlation coefficient with respect to the radial and tangential components of velocity fluctuation, it is found that the intermittent stall as well as the developed rotating stall are triggered by the interaction between the reverse flow in the diffuser entry region and the jet-wake like flow discharged from the impeller.
AB - In order to clarify the transient behavior from the non-stall condition to the developed rotating stall in vaneless diffuser of a centrifugal blower, blade-to-blade variations of velocity and wall pressure were measured immediately upstream and downstream of the impeller exit as well as in the vaneless diffuser by means of the semiconductor laser 2-focus velocimeter and the pressure sensor respectively. The specified auto-correlation coefficient of large scale disturbances with the wavelength larger than twice of the blade spacing show that the intermittent stall occurs prior to the developed rotating stall. By analyzing the flow-fluctuationellipse and the correlation coefficient with respect to the radial and tangential components of velocity fluctuation, it is found that the intermittent stall as well as the developed rotating stall are triggered by the interaction between the reverse flow in the diffuser entry region and the jet-wake like flow discharged from the impeller.
UR - http://www.scopus.com/inward/record.url?scp=65949088295&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=65949088295&partnerID=8YFLogxK
U2 - 10.1115/2000-GT-0467
DO - 10.1115/2000-GT-0467
M3 - Conference contribution
AN - SCOPUS:65949088295
T3 - Proceedings of the ASME Turbo Expo
BT - Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME Turbo Expo 2000: Power for Land, Sea, and Air, GT 2000
Y2 - 8 May 2000 through 11 May 2000
ER -