Data processing techniques for measurements collected from a single slanted hot-wire for turbomachinery applications

Reid A. Berdanier, Nicole L. Key

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The single slanted hot-wire technique has been used extensively as a method for measuring three velocity components in turbomachinery applications. The cross-flow orientation of probes with respect to the mean flow in rotating machinery render multiplewire probes subject to detrimental prong interference effects. As a result, the single slanted hot-wire technique is often preferred. Typical data reduction techniques solve a set of nonlinear equations determined by curve fits to calibration data. A new method is proposed which utilizes a look-up table method applied to a simulated triple wire sensor. Using experimental data collected from a multi-stage research compressor, results using these two data processing techniques are compared. Consideration is given to the experimental error which accompanies each data reduction process. Specific discussion regarding corrections for temperature and density changes present in a multistage compressor application is also included.

Original languageEnglish (US)
Title of host publication45th AIAA Fluid Dynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103629
DOIs
StatePublished - 2015
Event45th AIAA Fluid Dynamics Conference, 2015 - Dallas, United States
Duration: Jun 22 2015Jun 26 2015

Publication series

Name45th AIAA Fluid Dynamics Conference

Other

Other45th AIAA Fluid Dynamics Conference, 2015
Country/TerritoryUnited States
CityDallas
Period6/22/156/26/15

All Science Journal Classification (ASJC) codes

  • Engineering (miscellaneous)
  • Aerospace Engineering

Fingerprint

Dive into the research topics of 'Data processing techniques for measurements collected from a single slanted hot-wire for turbomachinery applications'. Together they form a unique fingerprint.

Cite this