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.

*This work was sponsored by the Air Force Office of Scientific Research, AFOSR, under grant/contract number FA9550-22-1-0021. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the Air Force Office of Scientific Research or the U.S. Government.

Publication: A Computational Fluid Dynamics Model of Shockwave Initiated Combustion, RW Forehand, MP Kinzel
AIAA AVIATION 2022 Forum, 3842, 2022
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