Title of article :
Vortex Analysis of Intra-Aneurismal Flow in Cerebral Aneurysms
Author/Authors :
Sunderland, Kevin Department of Biomedical Engineering - Michigan Technological University - Houghton, USA , Haferman, Christopher Department of Biomedical Engineering - Michigan Technological University - Houghton, USA , Chintalapani, Gouthami Siemens Medical Solution USA - Heffernan Estate, USA , Jiang, Jingfeng Department of Biomedical Engineering - Michigan Technological University - Houghton, USA
Pages :
16
From page :
1
To page :
16
Abstract :
This study aims to develop an alternative vortex analysis method by measuring structure ofIntracranial aneurysm (IA) flow vortexes across the cardiac cycle, to quantify temporal stability of aneurismal flow. Hemodynamics were modeled in “patient-specific” geometries, using computational fluid dynamics (CFD) simulations. Modified versions of known 𝜆2 and 𝑄-criterion methods identified vortex regions; then regions were segmented out using the classical marching cube algorithm. Temporal stability was measured by the degree of vortex overlap (DVO) at each step of a cardiac cycle against a cycle-averaged vortex and by the change in number of cores over the cycle. No statistical differences exist in DVO or number of vortex cores between 5 terminal IAs and 5 sidewall IAs. No strong correlation exists between vortex core characteristics and geometric or hemodynamic characteristics of IAs. Statistical independence suggests this proposed method may provide novel IA information. However, threshold values used to determine the vortex core regions and resolution of velocity data influenced analysis outcomes and have to be addressed in future studies. In conclusions, preliminary results show that the proposed methodology may help give novel insight toward aneurismal flow characteristic and help in future risk assessment given more developments.
Keywords :
Vortex Analysis , Intra-Aneurismal , DVO , CFD
Journal title :
Computational and Mathematical Methods in Medicine
Serial Year :
2016
Full Text URL :
Record number :
2606408
Link To Document :
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