实验流体力学
實驗流體力學
실험류체역학
JOURNAL OF EXPERIMENTS IN FLUID MECHANICS
2014年
3期
104-109
,共6页
李业军%王钊%田宝贤%梁晶%韩茂兰%陆泽%汤秀章
李業軍%王釗%田寶賢%樑晶%韓茂蘭%陸澤%湯秀章
리업군%왕쇠%전보현%량정%한무란%륙택%탕수장
KrF准分子激光%高速飞片%冲击波平面性%速度干涉条纹%侧向阴影照相
KrF準分子激光%高速飛片%遲擊波平麵性%速度榦涉條紋%側嚮陰影照相
KrF준분자격광%고속비편%충격파평면성%속도간섭조문%측향음영조상
KrF excimer laser pulse%high-speed flyer%shock wave plane character%velocity in-terferometer system for any reflector%side-on shadowgraph
利用诱导空间非相干技术平滑的KrF准分子(248nm)激光驱动带有烧蚀层的平面靶,研究激光空间均匀性对产生完整飞片的影响,结果表明激光不均匀性在2%以下,能够产生完整的高速飞片,且完整飞片能够维持20ns以上不破裂;当激光不均匀性达到5%,激光引入流体力学不稳定性种子应很强,冲击波在靶内输运过程中不稳定性不断发展增强,到靶背时强到足以使飞片解体甚至气化,不能产生完整的飞片。为了获得尽可能高的飞片速度,采用激光与烧蚀层参数不匹配方法,使冲击波对飞片作多次加速。利用功率密度为1012 W/cm2的KrF激光与含50μm Kapton烧蚀层的5μm铝飞片作用,得到速度约10km/s的高速飞片,与模拟结果吻合得很好。
利用誘導空間非相榦技術平滑的KrF準分子(248nm)激光驅動帶有燒蝕層的平麵靶,研究激光空間均勻性對產生完整飛片的影響,結果錶明激光不均勻性在2%以下,能夠產生完整的高速飛片,且完整飛片能夠維持20ns以上不破裂;噹激光不均勻性達到5%,激光引入流體力學不穩定性種子應很彊,遲擊波在靶內輸運過程中不穩定性不斷髮展增彊,到靶揹時彊到足以使飛片解體甚至氣化,不能產生完整的飛片。為瞭穫得儘可能高的飛片速度,採用激光與燒蝕層參數不匹配方法,使遲擊波對飛片作多次加速。利用功率密度為1012 W/cm2的KrF激光與含50μm Kapton燒蝕層的5μm鋁飛片作用,得到速度約10km/s的高速飛片,與模擬結果吻閤得很好。
이용유도공간비상간기술평활적KrF준분자(248nm)격광구동대유소식층적평면파,연구격광공간균균성대산생완정비편적영향,결과표명격광불균균성재2%이하,능구산생완정적고속비편,차완정비편능구유지20ns이상불파렬;당격광불균균성체도5%,격광인입류체역학불은정성충자응흔강,충격파재파내수운과정중불은정성불단발전증강,도파배시강도족이사비편해체심지기화,불능산생완정적비편。위료획득진가능고적비편속도,채용격광여소식층삼수불필배방법,사충격파대비편작다차가속。이용공솔밀도위1012 W/cm2적KrF격광여함50μm Kapton소식층적5μm려비편작용,득도속도약10km/s적고속비편,여모의결과문합득흔호。
KrF excimer laser (248nm)has high spatial uniformity by using induced spatial in-coherence technology.After image relay and amplification by optical angular multiplexing tech-nology,non-uniformity of image surface of focal spot is 1 .6%.The spot spatial uniformity decreases with increasing distance of deviating image surface,the spatial non-uniformity is up to 5% at 3mm place deviating image surface.Laser directly drives planar target with ablation layer, the effects of laser spatial uniformity on flyer planarity and integrity were investigated.The results show when the non-uniformity of laser is below 2%,the integrity of inference fringes measured by laser velocity interferometer system for reflector keeps very well,the inference frin-ges last about 20ns after fringes jump.And the flyer can fly about 150 microns.The roughness of discontinuity is 62ps,which indicates that the shock wave planarity is good.The target debris deposited on sputtering film from the target of about 120mm is larger particles,which confirms the flyer has better integrity.When the laser non-uniformity is 5%,the interference fringes dis-appear completely after fringes jump,and the target debris deposited on sputtering film becomes powder,which indicates the shock wave planarity is very poor under this laser condition.The experimental results show hydrodynamic instability seed is weak at good condition of the uni-formity of laser,the development of shock waves is not strong enough to make the flyer disinte-gration when shock waves transfer from the front surface to rear of larget.When the laser non-uniformity is about 5%,hydrodynamic instability seed driven by laser is very strong.When the shock wave transferred to the target back,hydrodynamic instability develops strong enough to make the flyer disintegration even gasification,which leads to the disappearance of interference fringes.So shock planarity driven by laser is strongly dependent on the laser beam spatial uni-formity,and the planarity and integrity of flyers depend on the shock planarity.According to the simulation results using one dimensional HYADES program,the ablation layer thickness should be reduced in order to improve the velocity of flyer.At the condition of thinner ablation layer,la-ser and ablation parameters do not match,shock waves driven by laser can accelerate the flyer multi-times.KrF laser with power density of about 1012 W/cm2 drove flat target of 5μm aluminum with 50μm Kapton ablation.Flyer trajectory was obtained using side-on shadowgraph.The curves of flyer velocity and acceleration were obtained by fitting the trajectory curve.Acceleration reaches 0.23×109km/s2,the velocity of flyer is about 9.8km/s.And the HYADES simulation shows there are 4 acceleration processes,the flyer velocity is about 10km/s.The results of experiment and simulation agreed very well.At the same conditions,simulations also show when the abla-tion thickness decreases to 30μm,the flyer velocity can be up to 16.5km/s.Target debris from backward jet maybe pollutes the laser focusing system components for too thin ablation.These all need to be verified by experiments.