@inproceedings{97479c38e71c4c789e615dbb1589d0af,
title = "The reynolds number effect on receptivity to a localized disturbance in a hypersonic boundary layer",
abstract = "Direct Numerical Simulations of wave packets in hypersonic flat–plate boundary layer reveal that the structure of a wave packet generated by a localized pulse disturbance introduced through a small hole in the wall depends on the location of the disturbance source. The wave packet develops both two–dimensional and three–dimensional structures when the disturbance source is located closer to the leading edge, whereas it has predominantly a two–dimensional nature when the disturbance source is located farther downstream (the Reynolds number effect). Theoretical analysis of the boundary–layer receptivity explains the Reynolds number effect by the different sensitivity of the flow to the first and the second discrete modes at the different disturbance source locations.",
author = "Jayahar Sivasubramanian and Anatoli Tumin and Fasel, {Hermann F.}",
note = "Publisher Copyright: {\textcopyright} 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 8th AIAA Flow Control Conference, 2016 ; Conference date: 13-06-2016 Through 17-06-2016",
year = "2016",
doi = "10.2514/6.2016-4246",
language = "English (US)",
isbn = "9781624104329",
series = "8th AIAA Flow Control Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "8th AIAA Flow Control Conference",
}