@inproceedings{c86c08f43bee4628a4c3f232030458b3,
title = "Flow structure identification in the near wake of an axisymmetric supersonic base flow using MEEMD",
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.",
author = "Koll, {Matthew D.} and Favale, {James V.} and Kirchner, {Branden M.} and Elliott, {Gregory S.} and Dutton, {J. Craig}",
note = "Publisher Copyright: {\textcopyright} 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 47th AIAA Fluid Dynamics Conference, 2017 ; Conference date: 05-06-2017 Through 09-06-2017",
year = "2017",
doi = "10.2514/6.2017-3972",
language = "English (US)",
isbn = "9781624105005",
series = "47th AIAA Fluid Dynamics Conference, 2017",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "47th AIAA Fluid Dynamics Conference, 2017",
}