Coupled investigation on drag and heat flux reduction over spiked waverider with a wide-speed range

Author:

Meng Yu-shan,Yan Li,Huang WeiORCID,Zhao Zhen-tao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

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4. Heat flux reduction mechanism induced by a combined opposing jet and cavity concept in supersonic flows;Huang;Acta Astronaut.,2016

5. Parametric study on the heat transfer of a blunt body with counterflowing jets in hypersonic flows;Guo;Int. J. Heat Mass Tran.,2018

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