Fundamental Performance of Disk-shaped Magnetohydrodynamics Accelerator

被引:0
作者
Takeshita, Shinji [1 ]
Buttapeng, Chainarong [2 ]
Furuya, Seizo [3 ]
Harada, Nobuhiro [1 ]
机构
[1] Nagaoka Univ Technol, Nagaoka, Niigata 94021, Japan
[2] Univ Thai Chamber Commerce, Bangkok, Thailand
[3] Gunma Univ, Maebashi, Gunma 371, Japan
关键词
Magnetohydrodynamics; Disk-shaped; Space Propulsion; Numerical Simulation; Air Plasma;
D O I
10.2322/tjsass.54.1
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper investigates the acceleration performance of a disk-shaped magnetohydrodynamics (MHD) accelerator. Quasi-1-dimensional (Q1D) numerical simulation employing the MacCormack scheme was developed. For the longer channel length of 0.9 m, thermal loss was estimated at over 60% and effective acceleration could not be achieved owing to large heat loss and large friction loss. For shorter channel lengths, thermal loss can be reduced below 20% owing to the smaller heat and the friction losses. However, with too short a channel length, accelerator performance was decreased by the MHD compression due to excessive Faraday current density. The effect of ratio of cross sectional area on performance was also studied. For a larger area ratio, the gas can be accelerated smoothly throughout the MHD channel. However, for the excessive expansion case of a sevenfold channel, gas velocity near the exit decreased due to transition to a "generator mode". For the best acceleration performance, the design channel length should be as short as possible preventing compression at the channel inlet. The area ratio should be large enough to prevent the compression but not too large, to prevent transition to a "generator mode".
引用
收藏
页码:1 / 6
页数:6
相关论文
共 10 条
[1]  
Cole J.W., 2002, 33 AIAA PLASM LAS C
[2]  
HARDIANTO T, 2007, 38 AIAA PLASM LAS C
[3]  
LINEBERRY J, 2006, 37 AIAA PLASM LAS C
[4]  
LITCHFORD R, 2007, 38 AIAA PLASM LAS C
[5]  
MACCORMACK RW, 2007, 45 AIAA AER SCI M
[6]  
MACCORMACK RW, 2006, 37 AIAA PLASM LAS C
[7]  
MOELLER T, 2008, 39 PLASM LAS C
[8]  
SAKAMOTO N, 2006, 37 AIAA PLASM LAS C
[9]  
TAKANO K, 1989, 11 S EFF US EN DIR E, P173
[10]  
TAKESHITA S, 2007, 45 AIAA AER SCI M EX