@inproceedings{3cb728161a824bb091c90757190ab06f,
title = "On the Unsteadiness of a Hypersonic Flow over an Axisymmetric Double Cone using Kinetic Methods",
abstract = "Hypersonic flows over an axisymmetric double cone was considered at M=6 for several Reynolds numbers. For the higher Reynolds number cases the flow is observed to be highly unsteady with a large separation bubble and several shocks. As the Reynolds number is reduced this unsteadiness disappears, as expected. A comparison with a M=16 case at the same Reynolds number from our earlier study showed that for M=6 case the flowfields are much more complex with a larger separation bubble and unsteady shock structures.",
author = "Karpuzcu, {Irmak T.} and Levin, {Deborah A.} and Vassilis Theofilis",
note = "The research conducted in this paper is supported by the Office of Naval Research under Grant No. N000141202195 titled \u201CMulti-scale modeling of unsteady shock-boundary layer hypersonic flow instabilities,\u201D with Dr. Eric Marineau as the Program Officer. This research is also supported by NSF ACCESS (previously XSEDE) Frontera supercomputer with the project number CTS22009.; AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 ; Conference date: 12-06-2023 Through 16-06-2023",
year = "2023",
doi = "10.2514/6.2023-3289",
language = "English (US)",
isbn = "9781624107047",
series = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023",
}