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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.

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

  • Reed W Forehand

    University of Central Florida

Authors

  • Reed W Forehand

    University of Central Florida

  • Khanh C Nguyen

    University of Central Florida

  • Sydney Briggs

    University of Central Florida

  • Nicolas Berube

    University of Central Florida

  • Caroline J Anderson

    University of Central Florida

  • Michael P Kinzel

    University of Central Florida, university of central florida

  • Subith Vasu

    University of Central Florida

  • Sheryl M Grace

    Boston University