Effect of inlet diameter on the flow structure and performance for aluminum-based water-jet engine

Author:

Xu Wei1,Bao WenChun2,Fang Zhe2,Zhang YunTian3,Liu YuanShu3,Ding GuoYu3,Yan PingHua4,Xu ChaoQi3

Affiliation:

1. ChengDu Aeronautic Polytechnic , Sichuan Province , Chengdu 610100 , People’s Republic of China

2. Beijing Institute of Astronautical Systems Engineering , Beijing 100076 , People’s Republic of China

3. State Key Laboratory for Strength and Vibration of Mechanical Structures, Shaanxi Engineering Laboratory for Vibration Control of Aerospace Structures, School of Aerospace , Xi’an Jiaotong University , Xi’an 710049 , People’s Republic of China

4. Department of Public Education , Jiangxi University of Applied Science , Nanchang 330100 , People’s Republic of China

Abstract

Abstract In this study, the flow field and performance for the aluminum based water ramjet was analyzed through numerical simulation. The time decrease in evaporation heat absorption process expands the range of aluminum/water combustion and increase the specific impulse. If the diameter of atomized water droplets from the primary inlet is large, the evaporation efficiency will be further reduced, which is not conducive to the further propagation of the reaction. However, if the diameter is small, the flow field temperature will be rapidly dropped due to rapid evaporation, and a large range of low-temperature areas will appear in the reaction area of the combustor. The diameter reduction of atomized water droplets from the secondary water inlet is conducive to the diffusion of the reaction area downstream, further and makes the combustion range be expanded. This effect is benefit for increasing the specific impulse and can reduce the temperature near the wall.

Publisher

Walter de Gruyter GmbH

Reference16 articles.

1. Miller, TF, Herr, JD. Green rocket propulsion by reaction of Al and Mg powders and water. In: AIAA 2004-4037; 2004.

2. Risha, GA. Combustion of aluminum particles with steam and liquid water. In: AIAA 2006-1154; 2006.

3. Kiely, DH. Review of underwater thermal propulsion. In: AIAA 94-2837; 1994:21–5 pp.

4. Branstetter, JR. Combustion properties of aluminum as ramjet fuel. Washington: Lewis Flight Propulsion Laboratory, National Advisory Commottee for Aeronautics; 1951.

5. Committee for Undersea weapons Science and Technology Naval Studies Board, Commission on Physical Sciences, Mathematics, and Applications National Research Council. An assessment of undersea weapons science and technology. Washington, DC: National Academy Press; 2000.

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