@inproceedings{339c0543e7f64edfa138a024727f056c,
title = "Application of a new shock-stable scheme for supersonic combustion flows",
abstract = "It is critical to implement accurate and appropriate numerical methods for understanding the combustion characteristics because of the strong interactions between an inviscid core flow and multiple near-wall viscous regions. A new numerical Godunov-type scheme, which is proposed and developed for the supersonic boundary layer simulations and the hypersonic viscous flow simulations, is extended to the supersonic combustion simulations because of its simpleness, robustness and efficiency. Numerical experiments including shock-induced combustion and fuel injection non-premixed combustion are tested and the results show good performance on the comparison to experiments data, especially for the prediction of ignition position. More numerical tests should be investigated to verify and validate on complex flows for the nest.",
keywords = "Ignition position, Shock-stable scheme, Supersonic combustion",
author = "Yongkang Zheng and Yue Zhou and Shusheng Chen and Chao Yan",
note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 ; Conference date: 22-07-2019 Through 25-07-2019",
year = "2019",
month = jul,
doi = "10.1109/ICMAE.2019.8880938",
language = "英语",
series = "2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "428--433",
booktitle = "2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019",
}