Effects of inflow parameters on thermal protection and drag reduction characteristics for hydrocarbon fueled supersonic film with combustion

Author:

Zuo Jingying,Zhang Silong,Wei Jianfei,Li Xin,Cui Naigang,Bao Wen

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Engineering (miscellaneous)

Reference33 articles.

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3. Research progress on active thermal protection for hypersonic vehicles;Zhang;Prog. Aero. Sci.,2020

4. Analysis and reduction of skin-friction in a rocket-based combined-cycle engine flow path operating from Mach 1.5 to 6.0;Wang;Acta Astronaut.,2018

5. Experimental investigation of isoenergetic film-cooling flows with shock interaction;Marquardt;AIAA J.,2019

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