Phase-averaged flow statistics in compressors using a rotated hot-wire technique
File(s)10.1007%2Fs00348-017-2326-x.pdf (5.04 MB)
Published version
Author(s)
Jelly, TO
Day, IJ
di Mare, L
Type
Journal Article
Abstract
A technique based on a rotated hot wire has been developed to characterise the unsteady, three-dimensional flow field between compressor blade rows. Data are acquired from a slanted hot wire rotated through a number of orientations at each measurement point. Phase-averaged velocity statistics are obtained by solving a set of sensor response equations using a weighted, non-linear regression algorithm. The accuracy and robustness of the method were verified a priori by conducting a series of tests using synthetic data. The method is demonstrated by acquiring a full set of phase-averaged flow statistics in the wake of a compressor stator blade row. The technique allows three components of phase-averaged velocity, six components of phase-averaged deterministic stress, and six components of phase-averaged Reynolds stress to be recovered using a single rotated hot-wire probe.
Date Issued
2017-05-01
Date Acceptance
2017-02-27
Citation
Experiments in Fluids, 2017, 58 (5)
ISSN
0723-4864
Publisher
Springer Verlag
Journal / Book Title
Experiments in Fluids
Volume
58
Issue
5
Copyright Statement
© The Author(s) 2017
This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.
This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.
License URL
Sponsor
Rolls-Royce Plc
Innovate UK
Grant Number
5002207858
RG68675
Subjects
Science & Technology
Technology
Engineering, Mechanical
Mechanics
Engineering
Hot-wire anemometry
Turbulence
Turbomachinery
TURBULENT SHEAR-FLOW
TURBOMACHINERY ROTORS
ORGANIZED WAVE
ANEMOMETRY
MECHANICS
STRESS
STAGE
PROBE
FIELD
FANS
Publication Status
Published
Article Number
48