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研究生: 劉昆妮
Liu, Kun-Ni
論文名稱: 次毫米尺度高密度氮氣氣靶之流體分析與其應用於雷射尾流場電子加速之特性研究
Fluid Analysis for Sub-Millimeter Dense Nitrogen Gas Targets Applicable to Laser Wakefield Acceleration
指導教授: 林明緯
Lin, Ming-Wei
口試委員: 陳仕宏
Chen, Shih-Hung
周紹暐
Chou, Shao-Wei
學位類別: 碩士
Master
系所名稱: 原子科學院 - 核子工程與科學研究所
Nuclear Engineering and Science
論文出版年: 2023
畢業學年度: 111
語文別: 中文
論文頁數: 75
中文關鍵詞: 雷射尾流場電子加速電漿粒子體模擬計算流體力學模擬
外文關鍵詞: Laser wakefield acceleration, Particle-in-cell simulation, Computational fluid dynamic simulation
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  • 雷射尾流場電子加速(laser wakefield acceleration, LWFA)可藉由聚焦具數兆瓦(terra watt, TW)尖峰功率之雷射脈衝至高密度薄氣體靶材達成。當雷射脈衝於密度高於1019 cm-3的電漿中傳播下,其強度即可因自聚焦(self-focusing)與自調變(self-modulation)等非線性效應而大幅增加而有效激發電漿波並加速電子至10 MeV等級之能量。除持續提升兆瓦級、高重複頻率雷射之技術,發展具適當空間分布、密度與成分之氣體靶材也有助於提升LWFA所產出電子數之特性,並得以應用於新型電子治療中或用以產生X光進行射線照相。因此本研究之重點即參考使用1 TW、40 fs的雷射脈衝進入次毫米長的高密度氮氣氣靶所產生之LWFA實驗結果,透過計算流體力學(computational fluid dynamic, CFD)模擬取得氣靶中氮原子的空間分佈,並將CFD模擬所得之氮原子密度分佈帶入電漿粒子體模擬(particle-in-cell simulation, PIC)以分析LWFA中雷射與電漿交互作用的物理機制以及所加速出的電子束特性。
    本研究建立450 μm長之氣腔的三維CFD模擬, 通入20 psi與25 psi之氮氣背壓,可分別得到具尖峰原子密度為7.6\times1018cm-3與9.5\times1018cm-3之分布,並透過PIC模擬可驗證在使用25 psi背壓時可相比於使用20 psi背壓下增加約1.5倍的電子束電荷,然而雷射脈衝在氣體密度較高時會因感受到較強的游離誘導折射(ionization-induced refraction)而具有一定程度散焦現象,進而導致電子束往橫向發散程度較高。本研究另於CFD模擬中對孔徑為178 μm的噴嘴建立二維軸對稱流體模型,並用以研究在馬赫數(Mach number)M\approx2.4之超音速噴流暫態模擬中,為滿足Courant-Friedrichs-Lewy條件(Courant-Friedrichs-Lewy condition, CFL condition)C_r\le1所需要的網格大小與時間步驟(time step),以及精進網格劃分與求解器設定使模擬數值收斂性提升。研究另建立二維x-y平面模型並於178 μm噴嘴上方引入刀片以調變氣體噴流密度分佈,在通入400 psi之氮氣背壓的條件下,以平面模型討論不同刀片對噴嘴的遮蓋率以及刀片幾何形狀對產生之氣體噴流密度下降梯度所造成的影響。由模擬結果可知改變刀片遮蓋率可調變密度下降坡長度L與密度下降梯度\frac{
    artial n}{
    artial x}。而模擬也顯示氣靶前端會因氣體經由刀片與噴嘴側的反彈而出現額外的次密度尖峰,此時改變刀片幾何形狀即有助於避免氣體反彈而造成的影響,使噴流分佈呈現單一密度尖峰並具有可調變的密度下降緩坡區間。


    Laser wakefield acceleration (LWFA) can be achieved by focusing a few-terawatt (TW) laser pulse into a thin gas target. When propagating in a plasma with an electron density >1019 cm-3,
    the pump pulse experiences nonlinear effects such as the self-focusing and the self-modulation that can result in a greatly increased laser intensity to excite plasma waves and generate 10-MeV-scale electrons from LWFA. In addition to inventing high-average-power, high-repetition-rate, TW-level lasers, developing gas target with a modified density profile, an increased density, or an appropriate gas component also opens up opportunities to enhance further the properties of output electron beams from LWFA and facilitate their downstream application in electron therapy and X-ray radiography. Therefore, based on the experimental results acquired by introducing 1-TW, 40-fs pulses into a sub-mm, dense nitrogen gas target, this work focuses on developing computational fluid dynamics (CFD) simulations to investigate the density distributions of nitrogen atoms in the target, which can be subsequently applied into particle-in-cell (PIC) simulations for resolving the process of LWFA and the characteristics of the accelerated electrons.
    Three-dimensional CFD model was first developed to study the distribution of nitrogen atom density inside a 450-μm-long gas cell, which showed that the peak atom density reached 7.6\times1018cm-3 and 9.5\times1018cm-3, respectively, when backing pressures of 20 and 25 psi were applied. The associated PIC simulations then indicated that the 25% increase in nitrogen atom density inside the cell could lead to a 1.5-fold increase of charge for the output electron beam but with a trade-off in a beam divergence.
    This study also developed two-dimensional CFD model in axisymmetric geometry for simulating gas jets produced from a 178-μm-diameter. This model was applied for optimizing the mesh size and the time step set in the simulation to satisfy the Courant-Friedrichs-Lewy (CFL) condition C_r<1 under the supersonic flow regime with a Mach number M\approx2.4, along with the modifications for the mesh refinement and the solver to substantially improve the convergence of the numerical results.
    With a two-dimensional planar geometry (in x and y coordinates), the CFD simulations were extended to study gas jets with a modulated density profile achieved by placing a blade above a nozzle; whereby length L of the density down-ramp region of the gas jet and the density gradient \frac{
    artial n}{
    artial x} across this region can be varied by tuning the blade coverage with respect to the nozzle. The results also showed that the multiple reflections of gas flows between the blade and the nozzle lip could result in the appearance of an extra density peak located prior to the main peak of the gas jet, which can be avoided by changing the geometry of the blade.

    摘要 ii Abstract iv 致謝 vi 目錄 vii 表目錄 x 圖目錄 xi 第一章 緒論 1 1.1 雷射電漿電子加速器簡介與發展 1 1.2 研究規劃 2 第二章 雷射尾流場電子加速原理 4 2.1 雷射脈衝的電場 4 2.2 電漿波的產生 5 2.2.1 雷射在電漿中的作用 5 2.2.2 LWFA中電子加速的條件 7 2.3 雷射脈衝的非線性效應 8 2.3.1 雷射自我聚焦效應(Self-focusing effect) 8 2.3.2 雷射自我調變機制(Self-modulated instability) 10 2.4 電子注入機制 10 2.4.1 電子自注入機制(Self-injection) 11 2.4.2 密度陡坡電子注入機制(Down ramp injection) 11 2.4.3 游離誘導電子注入機制(Ionization-induced injection) 12 2.5 LWFA電子加速限制 13 2.5.1 電子相移長度(Dephasing length) 13 2.5.2 雷射脈衝耗散長度(Laser pump depletion length) 14 2.6 數兆瓦LWFA與次兆瓦LWFA操作條件比較 15 2.7 電子束負載效應(BEAM LOADING EFFECT) 16 2.8 LWFA實驗中常用之氣體靶材 17 2.8.1 噴嘴(Gas jet) 17 2.8.2 氣腔(Gas cell) 19 2.8.3 毛細管波導(Capillary waveguide) 19 第三章 模擬工具與簡介 22 3.1 計算流體力學模擬 22 3.2 電漿粒子體模擬概述 22 第四章 氣腔CFD模擬與PIC模擬 24 4.1 CFD模擬模型與結果 24 4.1.1 三維幾何建模 24 4.1.2 計算網格設計 25 4.1.3 求解器與紊流模型設定 27 4.1.4 邊界條件設定 28 4.1.5 暫態模擬時序設計 29 4.1.6 氣體密度分布模擬結果 30 4.2 氣腔靶材之1 TW雷射尾流場電子加速之PIC模擬 32 4.2.1 模擬空間與網格 32 4.2.2 氣靶分布定義 32 4.2.3 雷射脈衝參數設定 33 4.2.4 模擬結果與討論 34 第五章 噴嘴CFD模擬 40 5.1 噴嘴CFD模擬模型與結果 40 5.1.1 次毫米寬氣體噴嘴下之次兆瓦 LWFA實驗摘要 40 5.1.2 氣體噴流之相關CFD模擬結果介紹與驗證 41 5.1.3 二維軸對稱幾何建模、網格設計、邊界條件與求解器設定 44 5.1.4 暫態數值收斂測試並將結果與實驗量測數值比較 46 5.1.5 改良網格劃分與求解器設定以提升模擬結果收斂性 50 5.2 密度陡坡氣體靶材CFD模擬模型與結果 53 5.2.1 密度陡坡氣體靶材之次兆瓦 LWFA實驗摘要 53 5.2.2 二維平面幾何建模、網格設計、邊界條件與求解器設定 56 5.2.3 暫態模擬中刀片遮蓋率對氣靶位置的影響與密度變化 59 5.2.4 刀片幾何對氣靶分布的影響 64 第六章 結論與未來規劃 67 6.1 結論 67 6.1.1 透過CFD模擬與PIC模擬對次毫米尺度噴嘴與氣腔分析結論 67 6.1.2 理想次毫米尺度氣靶設計 68 6.2 未來規劃 69 參考文獻 72

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