航空学报
航空學報
항공학보
ACTA AERONAUTICA ET ASTRONAUTICA SINICA
2010年
1期
88-92
,共5页
黄辉%金星%李倩%曹正蕊
黃輝%金星%李倩%曹正蕊
황휘%금성%리천%조정예
激光推进%管中激光加速器%光线追踪法%能量源项%数值模拟
激光推進%管中激光加速器%光線追蹤法%能量源項%數值模擬
격광추진%관중격광가속기%광선추종법%능량원항%수치모의
laser propulsion%laser-driven in-tube accelerator%ray tracking method%energy source term%numerical simulation
管中激光加速器是一种新型的激光推力器,弹射体在管道中被加速.利用光线追踪法,根据光线在网格中的传播路径信息,运用辐射输运方程,得到流场的能量源项;数值求解含能量源项的流体控制方程,对管道中等离子体流场激波的形成和演化过程进行了研究.模型能够模拟空气光学击穿、空气对激光能量的吸收、等离子体对激光的屏蔽作用和推力形成过程,通过计算得到冲量耦合系数为3.61×10~(-4) N/MW,等离子体内能转化为流场动能的比例约为9%.
管中激光加速器是一種新型的激光推力器,彈射體在管道中被加速.利用光線追蹤法,根據光線在網格中的傳播路徑信息,運用輻射輸運方程,得到流場的能量源項;數值求解含能量源項的流體控製方程,對管道中等離子體流場激波的形成和縯化過程進行瞭研究.模型能夠模擬空氣光學擊穿、空氣對激光能量的吸收、等離子體對激光的屏蔽作用和推力形成過程,通過計算得到遲量耦閤繫數為3.61×10~(-4) N/MW,等離子體內能轉化為流場動能的比例約為9%.
관중격광가속기시일충신형적격광추력기,탄사체재관도중피가속.이용광선추종법,근거광선재망격중적전파로경신식,운용복사수운방정,득도류장적능량원항;수치구해함능량원항적류체공제방정,대관도중등리자체류장격파적형성화연화과정진행료연구.모형능구모의공기광학격천、공기대격광능량적흡수、등리자체대격광적병폐작용화추력형성과정,통과계산득도충량우합계수위3.61×10~(-4) N/MW,등리자체내능전화위류장동능적비례약위9%.
Laser-driven in-tube accelerator is a new-style laser propulsion thruster characterized by accelerating projectile in a tube. With the ray tracking method, tracks of the rays in the grid are used to compute the energy source term by radiation transfer equation. The control equations with energy source term are solved numerically, through which the features of the generation and evolvement of the laser-induced shock waves in the tube are studied. Processes including air optical breakdown, absorption of laser energy, plasma shielding of the laser beam and thrust forming are reproduced. Numerical results indicate that the obtained momentum coupling coefficient is 3.61×10~(-4) N/MW,and the conversion efficiency of plasma internal energy to fluid kinetic energy is about 9%.