Numerical study on solid-fuel scramjet combustor with fuel-rich hot gas

Author:

Zhao Xiang,Xia Zhi-xun,Liu Bing,Lv Zhong,Ma Li-kunORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Passive zero-boil-off storage of liquid hydrogen for a long time in space;Sun;Int. J. Hydrog. Energy,2015

2. F. Shelly, M. Charles, R. Ken, V. Randy, Hyper-X Mach 7 scramjet design, Ground test and flight results, in: 13th International Space Planes and Hypersonics Systems and Technologies Conference, AIAA Paper 2005-3322.

3. R. Rogers, A. Shih, N. Hass, Scramjet development tests supporting the Mach 10 flight of the X-43, in: 13th International Space Planes and Hypersonics Systems and Technologies Conference, AIAA Paper 2005-3351.

4. Experimental and computational study on combustion performance of a kerosene fueled dual-mode scramjet engine;Tian;Aerosp. Sci. Technol.,2015

5. Experimental study of vitiation effects on hydrogen/kerosene fueled supersonic combustor;Wang;Aerosp. Sci. Technol.,2017

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