@inproceedings{a806035f73c846abb696b1636659cd01,
title = "Numerical Modeling of Shock Induced Aerobreakup of a Droplet at High Reynolds and Weber Number",
abstract = "Shock/droplet interactions have been the focus of numerous experimental and numerical investigations due to the importance of understanding droplet physics in many aerospace engineering applications. This paper presents a status update on current modeling efforts for simulating shock/droplet interactions (primarily in 2D) using the open-source NGA2-MAST framework (https://github.com/desjardi/NGA2). 2D simulation results using NGA2 are compared to previously published numerical and experimental results for shock Mach numbers ranging from 1.18 to 2.50. This work will provide the foundation for future 3D modeling efforts of shock/droplet interactions with higher shock Mach numbers.",
author = "Andrew Sayad and Jason Rabinovitch and A. Dworzanczyk and Parziale, {N. J.}",
note = "Publisher Copyright: {\textcopyright} 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 ; Conference date: 12-06-2023 Through 16-06-2023",
year = "2023",
doi = "10.2514/6.2023-4249",
language = "English",
isbn = "9781624107047",
series = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023",
booktitle = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023",
}