In 2016 and 2017, SJ-10 and TG-2 satellites were launched. In this short paper, we report recent progress on the studies of manipulation of colloidal droplets and instability of thermocapillary convection in large Pra...In 2016 and 2017, SJ-10 and TG-2 satellites were launched. In this short paper, we report recent progress on the studies of manipulation of colloidal droplets and instability of thermocapillary convection in large Prandtl number liquid bridge that based on the space experiments boarding SJ-10 and TG-2 satellites,separately. It was shown that the colloidal droplets can be successfully formed and manipulated in microgravity through the patterned substrates. In another aspect, the coffee-ring effect was observed at the first time in space. For the studies of the instability of thermocapillary convection in large Prandtl number liquid bridge in microgravity, our experiments in TG-2 broadened the way of such kind of study and abundant experimental results are emerging.展开更多
The Cu2O/TiO2 p-n heterojunction composite photoelectrodes were prepared by depositing Cu 2 O nanoparticles on the surface of TiO 2 nanotubes via anodic oxidation and constant current deposition.Field emission scannin...The Cu2O/TiO2 p-n heterojunction composite photoelectrodes were prepared by depositing Cu 2 O nanoparticles on the surface of TiO 2 nanotubes via anodic oxidation and constant current deposition.Field emission scanning electron microscopy(SEM)and high-resolution transmission electron microscopy(HRTEM)analyses showed that Cu 2 O nanoparticles not only deposited on the surface of TiO 2 nanotube array,but also on the wall of TiO 2 nanotubes.The Cu 2 O deposition amount could be adjusted by changing the deposition time.The photoelectrochemical cathodic protection(PECCP)performance of the prepared photoelectrodes for 316L stainless steel(SS)was tested under visible light.The constant current deposition time had a signifi cant eff ect on the PECCP performance of Cu 2 O/TiO 2-X photoelectrodes and Cu 2 O/TiO 2-20 had the best PECCP performance for the coupled 316L SS.This was attributed to the appropriate amount and thickness of Cu 2 O to form p-n heterojunctions with TiO 2,in which separation of the photogenerated carriers was accelerated and transfer of the photogenerated electrons to 316L SS for PECCP was facilitated.展开更多
为研究靶板材料性能对爆炸成型弹丸(Explosively Formed Projectile,EFP)侵彻靶后破片特性的影响,开展EFP侵彻不同材料靶板(Q235钢、45号钢、装甲钢、2A12铝)后效破片特性试验,采用X光摄影方法观测靶后破片云形态及膨胀尺寸,通过布置多...为研究靶板材料性能对爆炸成型弹丸(Explosively Formed Projectile,EFP)侵彻靶后破片特性的影响,开展EFP侵彻不同材料靶板(Q235钢、45号钢、装甲钢、2A12铝)后效破片特性试验,采用X光摄影方法观测靶后破片云形态及膨胀尺寸,通过布置多层纤维板获得破片散布特性,并对靶后破片进行回收。研究结果表明:在靶板密度一定的情况下,靶板强度主要影响破片云轴向膨胀能力,对径向膨胀能力影响很小;靶后破片环形毁伤区的飞散角位于20°~25°范围内差别不大,但是靶板背面出口崩落会造成靶后破片飞散角出现极大值,随着钢靶强度的增大,靶后破片径向散布增强,破片总数减小,但是大质量段钢破片数量增多;不同强度钢靶产生的钢破片平均尺寸满足Kipp等提出的基于材料流动应力的碎片尺寸模型。展开更多
针对杆式爆炸成型侵彻体(Explosively formed penetrator, EFP)的侵彻能力问题,利用数值仿真手段开展杆式EFP侵彻特性研究,分析杆式EFP成型形态、着靶速度及材料特性对其侵彻能力的影响,得到杆式EFP成型特征参数在侵彻过程中的影响规律...针对杆式爆炸成型侵彻体(Explosively formed penetrator, EFP)的侵彻能力问题,利用数值仿真手段开展杆式EFP侵彻特性研究,分析杆式EFP成型形态、着靶速度及材料特性对其侵彻能力的影响,得到杆式EFP成型特征参数在侵彻过程中的影响规律。研究结果表明:杆式EFP在侵彻过程中,除初始阶段(碰撞后)和最后阶段(杆侵蚀后)外,弹体保持恒定速度运动,满足恒速杆假设;稳定侵彻时,随着密实部长度的逐渐减小,中空尾裙部材料不断流入密实部补充其侵蚀损失。增加弹体长度可以在一定程度上提高EFP的侵彻能力,但归一化侵彻深度下降;提高着靶速度和密实部长度可以显著提升杆式EFP侵彻性能。杆式EFP的强度对侵彻的影响有限,但靶体强度不可忽略,弹靶材料密度是影响侵彻体侵彻的主要因素。展开更多
针对三点起爆控制参数(起爆直径、起爆同步误差)对尾翼爆炸成型弹丸(explosively formed projectile,EFP)成型的影响问题,理论分析了三点起爆条件下爆轰波的马赫碰撞,计算获得了不同起爆直径下马赫波的相关参数,利用LS-DYNA有限元软件...针对三点起爆控制参数(起爆直径、起爆同步误差)对尾翼爆炸成型弹丸(explosively formed projectile,EFP)成型的影响问题,理论分析了三点起爆条件下爆轰波的马赫碰撞,计算获得了不同起爆直径下马赫波的相关参数,利用LS-DYNA有限元软件通过数值模拟研究了不同起爆直径下三点起爆同步误差对EFP尾翼成型及飞行速度的影响规律。结果表明,起爆直径越大,马赫波在药型罩上的作用面积越小,马赫超压越大,形成的EFP长径比和速度越大;起爆直径为30、40、50 mm三点起爆成型装药形成较佳尾翼EFP应满足的最大起爆同步误差分别为50、100、150ns;此外,尽量使中间起爆点起爆同步误差约为最大同步误差的一半,有利于降低尾翼EFP的侧向分速度,提高飞行稳定性。展开更多
文摘In 2016 and 2017, SJ-10 and TG-2 satellites were launched. In this short paper, we report recent progress on the studies of manipulation of colloidal droplets and instability of thermocapillary convection in large Prandtl number liquid bridge that based on the space experiments boarding SJ-10 and TG-2 satellites,separately. It was shown that the colloidal droplets can be successfully formed and manipulated in microgravity through the patterned substrates. In another aspect, the coffee-ring effect was observed at the first time in space. For the studies of the instability of thermocapillary convection in large Prandtl number liquid bridge in microgravity, our experiments in TG-2 broadened the way of such kind of study and abundant experimental results are emerging.
基金Supported by the National Natural Science Foundation of China(Nos.41576114,41676069)the State Key Laboratory for Marine Corrosion and Protection,Luoyang Ship Material Research Institute,China(No.614290101011703)the Qingdao Innovative Leading Talent Foundation(No.15-10-3-15-(39)-zch)。
文摘The Cu2O/TiO2 p-n heterojunction composite photoelectrodes were prepared by depositing Cu 2 O nanoparticles on the surface of TiO 2 nanotubes via anodic oxidation and constant current deposition.Field emission scanning electron microscopy(SEM)and high-resolution transmission electron microscopy(HRTEM)analyses showed that Cu 2 O nanoparticles not only deposited on the surface of TiO 2 nanotube array,but also on the wall of TiO 2 nanotubes.The Cu 2 O deposition amount could be adjusted by changing the deposition time.The photoelectrochemical cathodic protection(PECCP)performance of the prepared photoelectrodes for 316L stainless steel(SS)was tested under visible light.The constant current deposition time had a signifi cant eff ect on the PECCP performance of Cu 2 O/TiO 2-X photoelectrodes and Cu 2 O/TiO 2-20 had the best PECCP performance for the coupled 316L SS.This was attributed to the appropriate amount and thickness of Cu 2 O to form p-n heterojunctions with TiO 2,in which separation of the photogenerated carriers was accelerated and transfer of the photogenerated electrons to 316L SS for PECCP was facilitated.
文摘为研究靶板材料性能对爆炸成型弹丸(Explosively Formed Projectile,EFP)侵彻靶后破片特性的影响,开展EFP侵彻不同材料靶板(Q235钢、45号钢、装甲钢、2A12铝)后效破片特性试验,采用X光摄影方法观测靶后破片云形态及膨胀尺寸,通过布置多层纤维板获得破片散布特性,并对靶后破片进行回收。研究结果表明:在靶板密度一定的情况下,靶板强度主要影响破片云轴向膨胀能力,对径向膨胀能力影响很小;靶后破片环形毁伤区的飞散角位于20°~25°范围内差别不大,但是靶板背面出口崩落会造成靶后破片飞散角出现极大值,随着钢靶强度的增大,靶后破片径向散布增强,破片总数减小,但是大质量段钢破片数量增多;不同强度钢靶产生的钢破片平均尺寸满足Kipp等提出的基于材料流动应力的碎片尺寸模型。
文摘针对杆式爆炸成型侵彻体(Explosively formed penetrator, EFP)的侵彻能力问题,利用数值仿真手段开展杆式EFP侵彻特性研究,分析杆式EFP成型形态、着靶速度及材料特性对其侵彻能力的影响,得到杆式EFP成型特征参数在侵彻过程中的影响规律。研究结果表明:杆式EFP在侵彻过程中,除初始阶段(碰撞后)和最后阶段(杆侵蚀后)外,弹体保持恒定速度运动,满足恒速杆假设;稳定侵彻时,随着密实部长度的逐渐减小,中空尾裙部材料不断流入密实部补充其侵蚀损失。增加弹体长度可以在一定程度上提高EFP的侵彻能力,但归一化侵彻深度下降;提高着靶速度和密实部长度可以显著提升杆式EFP侵彻性能。杆式EFP的强度对侵彻的影响有限,但靶体强度不可忽略,弹靶材料密度是影响侵彻体侵彻的主要因素。
文摘针对三点起爆控制参数(起爆直径、起爆同步误差)对尾翼爆炸成型弹丸(explosively formed projectile,EFP)成型的影响问题,理论分析了三点起爆条件下爆轰波的马赫碰撞,计算获得了不同起爆直径下马赫波的相关参数,利用LS-DYNA有限元软件通过数值模拟研究了不同起爆直径下三点起爆同步误差对EFP尾翼成型及飞行速度的影响规律。结果表明,起爆直径越大,马赫波在药型罩上的作用面积越小,马赫超压越大,形成的EFP长径比和速度越大;起爆直径为30、40、50 mm三点起爆成型装药形成较佳尾翼EFP应满足的最大起爆同步误差分别为50、100、150ns;此外,尽量使中间起爆点起爆同步误差约为最大同步误差的一半,有利于降低尾翼EFP的侧向分速度,提高飞行稳定性。
