TY - GEN
T1 - Phase resolved hot-wire measurements for high speed turbomachinery flows
AU - Jaffa, Nicholas
AU - Morris, Scott
AU - Cameron, Joshua
N1 - Publisher Copyright:
© 2014 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2014
Y1 - 2014
N2 - Detailed measurements of total temperature and velocity in high-speed, rotating turbomachinery flows are difficult due to the high sensor frequency response required. Constant temperature hot-wires have the needed frequency response, but are sensitive to both Tt and effective wire ρU which vary significantly in high speed flows. The multiple overheat method can be used to decouple the phase locked averages of Tt and wire effective ρU from the phase locked average hot-wire voltages. The present study will demonstrate the efficacy of this technique as well as a detailed uncertainty analysis of the multiple overheat method. The overall uncertainty is primarily determined by: the quality of the hot-wire calibration, the frequency response of the constant temperature hot-wire system, and the ability of the turbomachinery facility to maintain a constant operating point while the hot-wire overheat values are changed. As a proof of concept, a single constant temperature hot-wire was operated at four different overheats at the exit of a transonic axial compressor rotor. The phase locked average Tt and wire effective ρU fields show flow features relative to the rotor including blade wakes and tip clearance flows. These phase locked average measurements were validated against each other.
AB - Detailed measurements of total temperature and velocity in high-speed, rotating turbomachinery flows are difficult due to the high sensor frequency response required. Constant temperature hot-wires have the needed frequency response, but are sensitive to both Tt and effective wire ρU which vary significantly in high speed flows. The multiple overheat method can be used to decouple the phase locked averages of Tt and wire effective ρU from the phase locked average hot-wire voltages. The present study will demonstrate the efficacy of this technique as well as a detailed uncertainty analysis of the multiple overheat method. The overall uncertainty is primarily determined by: the quality of the hot-wire calibration, the frequency response of the constant temperature hot-wire system, and the ability of the turbomachinery facility to maintain a constant operating point while the hot-wire overheat values are changed. As a proof of concept, a single constant temperature hot-wire was operated at four different overheats at the exit of a transonic axial compressor rotor. The phase locked average Tt and wire effective ρU fields show flow features relative to the rotor including blade wakes and tip clearance flows. These phase locked average measurements were validated against each other.
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U2 - 10.2514/6.2014-3437
DO - 10.2514/6.2014-3437
M3 - Conference contribution
AN - SCOPUS:84913533926
T3 - 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
BT - 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014
Y2 - 28 July 2014 through 30 July 2014
ER -