@inproceedings{e5220a6a84534fc88ad1043aafa5a3f5,
title = "Simulation of hypersonic shock-shock interaction over a hemisphere",
abstract = "The interaction of an oblique shock with the bow shock in front of a hemisphere in Mach 14.6 flow is examined. The hypersonic laminar simulation is performed using a C++ code with the implementation of MPI written by the authors. The simulation is based on a set of experiments performed at the 48-inch Shock Tunnel at Calspan University at Buffalo Research Center (CUBRC). The Edney III interaction exhibits a statistically stationary behavior with dominant Strouhal number of 0.346. The surface pressure coefficient and dimensionless heat transfer are in general agreement with experiment; however, the location of the interaction of the incident shock with the bow shock is evidently slightly different than in the experiment. More calculations are in progress.",
author = "Nadia Kianvashrad and Doyle Knight",
note = "Publisher Copyright: {\textcopyright} 2018 by Nadia Kianvashrad and Doyle Knight.; 48th AIAA Fluid Dynamics Conference, 2018 ; Conference date: 25-06-2018 Through 29-06-2018",
year = "2018",
doi = "10.2514/6.2018-3708",
language = "English (US)",
isbn = "9781624105531",
series = "2018 Fluid Dynamics Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "2018 Fluid Dynamics Conference",
}