Multi-Scale Modeling of a Shock Tube to Examine Shock-Droplet Interaction
ORAL
Abstract
This effort presents a multi-physics, multi-scale approach to modeling the problem of shock-droplet interaction within a shock tube. The overall motivation of this study is to simulate a practical experiment that provides a similar mechanism that a rain droplet would experience when interacting with the bow shock of a reentry vehicle. The present work presents a multi-scale approach using a lower fidelity simulation of the entire shock tube to gain the boundary conditions of the test section, and provide a preliminary impact analysis while a higher fidelity simulation of the droplet explores phenomena such as breakup, cavitation, and evaporation.
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Publication: A Computational Fluid Dynamics Model of Shockwave Initiated Combustion, RW Forehand, MP Kinzel<br>AIAA AVIATION 2022 Forum, 3842, 2022<br>Numerical Modeling of Shockwave Initiated Combustion of a Hydrogen-Oxygen Mixture Within a Shock Tube, RW Forehand, University of Central Florida Thesis, 2021
Presenters
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Reed W Forehand
University of Central Florida
Authors
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Reed W Forehand
University of Central Florida
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Khanh C Nguyen
University of Central Florida
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Sydney Briggs
University of Central Florida
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Nicolas Berube
University of Central Florida
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Caroline J Anderson
University of Central Florida
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Michael P Kinzel
University of Central Florida, university of central florida
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Subith Vasu
University of Central Florida
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Sheryl M Grace
Boston University