@Article{CiCP-18-1095,
author = {Ming-Chung Lo, Cheng-Chin Su, Jong-Shinn Wu and Kun-Chang Tseng},
title = {Modelling Rarefied Hypersonic Reactive Flows Using the Direct Simulation Monte Carlo Method},
journal = {Communications in Computational Physics},
year = {2018},
volume = {18},
number = {4},
pages = {1095--1121},
abstract = {<p style="text-align: justify;">This paper presents the implementation, validation and application of TCE
(total collision energy) model for simulating hypersonic reactive flows in a parallel
direct simulation Monte Carlo code, named PDSC<sup>++</sup>, using an unstructured grid. A
series of benchmarking test cases, which include reproduction of theoretical rate constants
in a single cell, 2D hypersonic flow past a cylinder and 2D-axisymmetric hypersonic
flow past a sphere, were performed to validate the implementation. Finally,
detailed aerothermodynamics of the flown reentry Apollo 6 Command Module at 105
km is simulated to demonstrate the powerful capability of the PDSC<sup>++ </sup>in treating
realistic hypersonic reactive flow at high altitude.</p>},
issn = {1991-7120},
doi = {https://doi.org/10.4208/cicp.080115.010515s},
url = {http://global-sci.org/intro/article_detail/cicp/11062.html}
}