Flow structure identification in the near wake of an axisymmetric supersonic base flow using MEEMD

Matthew D. Koll, James V. Favale, Branden M. Kirchner, Gregory S. Elliott, J. Craig Dutton

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

Abstract

The supersonic separated flowfield aft of a blunt-faced cylinder aligned with the freestream is highly complex. Therefore, new methods are needed to study this flowfield. Recently, empirical mode decomposition has emerged in the fluid dynamics community as a way to separate spatial and temporal scales in a signal. In this study, the multi-dimensional extension of ensemble empirical mode decomposition is used on the velocity fields obtained with particle image velocimetry of said flowfield. Multi-dimensional ensemble empirical mode decomposition was performed on both three-component planar and volumetric data sets. The analysis resulted in the scale separation of the different structures within the flowfield and revealed horseshoe-shaped and streamwise-oriented structures. This paper also presents the idea of eliminating small-scale features and noise from data sets by subtracting the corresponding small-scale components of multi-dimensional ensemble empirical mode decomposition from the original image.

Original languageEnglish (US)
Title of host publication47th AIAA Fluid Dynamics Conference, 2017
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105005
DOIs
StatePublished - 2017
Event47th AIAA Fluid Dynamics Conference, 2017 - Denver, United States
Duration: Jun 5 2017Jun 9 2017

Publication series

Name47th AIAA Fluid Dynamics Conference, 2017

Other

Other47th AIAA Fluid Dynamics Conference, 2017
Country/TerritoryUnited States
CityDenver
Period6/5/176/9/17

ASJC Scopus subject areas

  • Aerospace Engineering
  • Engineering (miscellaneous)

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