An efficient unstructured WENO method for supersonic reactive flows-Reference-Cited by-同舟云学术

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An efficient unstructured WENO method for supersonic reactive flows

Published:2018-03-15 Issue:4 Volume:34 Page:623-631
ISSN:0567-7718
Container-title:Acta Mechanica Sinica
language:en
Short-container-title:Acta Mech. Sin.

Author:

Zhao Wen-Geng,Zheng Hong-Wei,Liu Feng-Jun,Shi Xiao-Tian,Gao Jun,Hu Ning,Lv Meng,Chen Si-Cong,Zhao Hong-Da

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Link

http://link.springer.com/article/10.1007/s10409-018-0756-1/fulltext.html

Reference67 articles.

1. Roy, G.D.: Pulse detonation propulsion: challenges, current status, and future perspective. Prog. Energy Combust. 30, 545–672 (2004)

2. Geßner, T.: Dynamic mesh adaption for supersonic combustion waves modeled with detailed reaction mechanisms. [Ph.D. Thesis], Technical University Dresden, German (2001)

3. Fedkiw, R.P., Merriman, B., Osher, S.: High accuracy numerical methods for thermally perfect gas flows with chemistry. J. Comput. Phys. 132, 175–190 (1997)

4. Togashi, F., Löhner, R., Tsuboi, N.: Numerical simulation of H $$_2$$ 2 /air detonation using unstructured mesh. Shock Waves 192, 151–162 (2009)

5. Ju, Y.: Recent progress and challenges in fundamental combustion research. Adv. Mech. 44, 1142–1157 (2014)

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