@inproceedings{a9933664dbab4b9d9e5a5a59154968ec,
title = "Simulations of dynamic shock wave/boundary layer interactions using hpcmp createtm-av kestrel coffe",
abstract = "In this manuscript, simulations of a canonical hollow cylinder flare using HPCMP CREATETM-AV Kestrel Component COFFE are compared to experimental data taken in the University of Tennessee Space Institute TALon Mach 4 Ludwieg tube. Preliminary comparison is with time-resolved shadowgraph image sequences of simultaneous tripped and untripped flow and unsteady pressure sensitve paint measurements. Relevant features compared between experimental and computational data are the interaction angles, wave angles, separation distance, and flow field unsteadiness. Modeling approaches are unsteady with global time stepping for modeling the untripped configuration and steady with the Spalart-Allmaras (SA) one-equation turbulence model for modeling the tripped portion of the configuration. Initial results compare well with experiment based on measurements of the angles of relevant features and qualitative comparison.",
author = "Nutter, {Nicole F.} and Cobourn, {Jack W.} and Bond, {Ryan B.} and Phil Kreth and Schmisseur, {John D.} and Glasby, {Ryan S.} and Stefanski, {Douglas L.} and Ethan Hereth and Coder, {James G.}",
note = "Publisher Copyright: {\textcopyright} 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.; AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021 ; Conference date: 11-01-2021 Through 15-01-2021",
year = "2021",
language = "English (US)",
isbn = "9781624106095",
series = "AIAA Scitech 2021 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
pages = "1--14",
booktitle = "AIAA Scitech 2021 Forum",
}