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Modelling of Edge Plasma on JT-60U Tokamak by Using SOLPS5.0 Code
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作者 陈一平 H. KAWASHIMA +2 位作者 N. ASAKURA K. SHIMIZU H. TAKENAGA 《Plasma Science and Technology》 SCIE EI CAS CSCD 2011年第3期302-306,共5页
The edge transport code SOLPS5.0 is used to model edge plasmas in the experi- mental shots on JT-60U and the profiles of the transverse particle and heat transport coefficients D, Xe and Xi along the outer midplane ar... The edge transport code SOLPS5.0 is used to model edge plasmas in the experi- mental shots on JT-60U and the profiles of the transverse particle and heat transport coefficients D, Xe and Xi along the outer midplane are obtained by fitting the simulational results to the experimental data in L-mode shot 39090 and H-mode shots 37851, 37856. The modelling and fitting results show that within the pedestal region in H-mode shots 37851 and 37856 the radial particle transport coefficient D exhibits a significant drop, but, for L-mode shot 39090, the obvious drop in both D and Xe was not found. 展开更多
关键词 solps5.0 JT-60U MODELLING
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Simulation of Boundary Plasma for HCSB-DEMO by Using 2D Edge Plasma Transport Code SOLPS5.0
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作者 郑国尧 冯开明 +2 位作者 盛光昭 潘宇东 何宏达 《Plasma Science and Technology》 SCIE EI CAS CSCD 2010年第2期139-143,共5页
A simulation on HCSB-DEMO (helium-cooled solid breeder, HCSB) edge plasma, by using 2D edge plasma transport code SOLPS5.0, is presented. There is 400 MW heat power crossing CIB (core interface boundary). The heat... A simulation on HCSB-DEMO (helium-cooled solid breeder, HCSB) edge plasma, by using 2D edge plasma transport code SOLPS5.0, is presented. There is 400 MW heat power crossing CIB (core interface boundary). The heat flux profiles and peak flux at the divertor targets with different boundary densities axe investigated. It is indicated that the HCSB-DEMO divertor should operate at a proper upstream density in order to avoid a high heat flux at the divertor targets. When the upstream density is 0.63x 102~ m-3, the peak heat flux at the divertor targets will be above 17 MW/m2. The cross-field transport, the power crossing CIB and the power fraction taken by electrons and ions and SOL (scrape-off-layer) thickness are analyzed as unknown parameters. It is shown that the peak flux at the divertor target is very sensitive to these parameters. The simulation results will be used in the divertor design for HCSB-DEMO. 展开更多
关键词 solps5.0 upstream density heat flux
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Simulation Study for Divertor Geometry and Gas Puffing to Handle Huge Exhaust Power in HL-2M with SOLPS5.0
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作者 崔学武 潘宇东 +2 位作者 李佳鲜 张锦华 毛瑞 《Plasma Science and Technology》 SCIE EI CAS CSCD 2013年第6期489-492,共4页
One of the critical issues to be solved for HL-2M is the power exhaust.Divertor target plate geometry strongly influences the plasma profiles by controlling the neutral recycling pattern,which in turn has a strong eff... One of the critical issues to be solved for HL-2M is the power exhaust.Divertor target plate geometry strongly influences the plasma profiles by controlling the neutral recycling pattern,which in turn has a strong effect on the symmetry and stability of the divertor plasma and finally on the whole edge region.The numerical simulation SOLPS5.0 package is used to design and explore the divertor target plates for HL-2M.We start with the choice of a proper target plate geometry,which has a smaller incidence angle in the permissible space,and then discuss the method of gas puffing to reduce the heat flux density on the target and the effects of gas puffing on the divertor plasma performance. 展开更多
关键词 solps5.0 numerical simulation gas puffing
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HL-2M Divertor Geometry Exploration with SOLPS5.0
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作者 崔学武 潘宇东 +3 位作者 崔正英 李佳鲜 张锦华 毛瑞 《Plasma Science and Technology》 SCIE EI CAS CSCD 2013年第12期1184-1188,共5页
One of the critical issues to be solved for HL-2M is the power and particle exhaust. Divertor target plate geometry strongly influences the plasma profiles by controlling the neutral recycling pattern, which has in tu... One of the critical issues to be solved for HL-2M is the power and particle exhaust. Divertor target plate geometry strongly influences the plasma profiles by controlling the neutral recycling pattern, which has in turn a strong effect on the symmetry and stability of the divertor plasma and finally on the whole edge region. The numerical simulation software SOLPS5.0 Pack- age is used to design and explore the divertor target plates for HL-2M. We choose two divertor geometries, and assess the heat flux on the target plates and first wall, then further discuss the di- vertor plasma parameters, and how private flux baffling affects both neutral recirculation pattern and pumping efficiency. 展开更多
关键词 solps5.0 numerical simulation divertor geometry exploration
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Comparative Study of the SN, DDN and DN Diverter Plasma Simulations for HCSB-DEMO
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作者 郑国尧 冯开明 +2 位作者 盛光昭 潘宇东 何宏达 《Plasma Science and Technology》 SCIE EI CAS CSCD 2011年第1期26-29,共4页
A comparative study of SN (single null), DDN (disconnected double-null) and DN (double null) diverters for HCSB-DEMO (helium-cooled solid breeder, HCSB) is reported in this paper by using the 2D edge plasma tr... A comparative study of SN (single null), DDN (disconnected double-null) and DN (double null) diverters for HCSB-DEMO (helium-cooled solid breeder, HCSB) is reported in this paper by using the 2D edge plasma transport code SOLPS5.0. There is a heat power of 400 MW crossing CIB (core interface boundary). The peak heat flux at targets with different upstream densities is investigated. It is indicated that the peak heat flux at the outer target with a SN diverter is lower than that at the outer-down target with a DDN diverter under the same upstream density, but is higher than that at the outer target with a DN diverter. The diverter should operate at a proper upstremn density to avoid strong high heat flux at the targets. The peak heat flux at the targets and first wail are sensitive to the SOL (scrape-off-layer) grid thickness. The simulated results wilt provide data for the design of diverter in HCSB-DEMO. 展开更多
关键词 solps5.0. upstream density heat flux
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HL-2M常规偏滤器位形抽气对碳杂质分布影响的模拟分析
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作者 周月 郑国尧 +8 位作者 杜海龙 潘宇东 李佳鲜 薛雷 潘卫 黄文玉 薛淼 彭媛媛 曲成海 《核聚变与等离子体物理》 CAS CSCD 北大核心 2021年第2期97-104,共8页
在小角度V型结构的HL-2M常规偏滤器位形下,采用SOLPS 5.0程序研究了抽气速率S_(p)对装置粒子排除控制能力及溅射产生的碳杂质分布的影响。模拟结果表明,当进入边缘区域的能量为4MW、上游密度为n_(sep)=3.0×10^(19)m^(-3)靶板电子温... 在小角度V型结构的HL-2M常规偏滤器位形下,采用SOLPS 5.0程序研究了抽气速率S_(p)对装置粒子排除控制能力及溅射产生的碳杂质分布的影响。模拟结果表明,当进入边缘区域的能量为4MW、上游密度为n_(sep)=3.0×10^(19)m^(-3)靶板电子温度T_(e)的上升和表面材料溅射增强,导致有效电荷量Z_(eff)升高。在抽气速率约为20~40m^(3)·s^(-1)时,常规偏滤器的粒子排除效率较高。 展开更多
关键词 SOLPS 5.0 偏滤器位形 粒子控制 热负载 有效电荷量Z_(eff)
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东方超环托卡马克高约束模式边界等离子体输运数值模拟研究 被引量:5
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作者 杜海龙 桑超峰 +6 位作者 王亮 孙继忠 刘少承 汪惠乾 张凌 郭后扬 王德真 《物理学报》 SCIE EI CAS CSCD 北大核心 2013年第24期229-238,共10页
利用SOLPS5.0模拟研究东方超环托卡马克(EAST)高约束模式时的刮削层等离子体.在高约束模式放电实验参数(第36291炮)的限制下,通过调整上游区径向反常输运系数来实现高约束模式模拟,在上游电子密度和温度与实验符合的条件下能够很好地进... 利用SOLPS5.0模拟研究东方超环托卡马克(EAST)高约束模式时的刮削层等离子体.在高约束模式放电实验参数(第36291炮)的限制下,通过调整上游区径向反常输运系数来实现高约束模式模拟,在上游电子密度和温度与实验符合的条件下能够很好地进行下游区模拟.在实现高约束模拟的基础上又分别研究了漂移项对偏滤器靶板能流不对称性的影响和上游能流衰减宽度对靶板能流密度峰值的影响.通过模拟发现,漂移是导致EAST放电内外靶板不对称性的主要原因,增大上游能流衰减宽度可以明显降低入射到靶板的峰值热流,并且偏滤器区辐射以及与中性粒子的相互作用减小了能流的衰减宽度对达到靶板能流的影响. 展开更多
关键词 托卡马克 高约束模式 SOLPS5 0 漂移
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