实验流体力学
實驗流體力學
실험류체역학
JOURNAL OF EXPERIMENTS IN FLUID MECHANICS
2014年
3期
93-97
,共5页
充水压力容器%超高速撞击%风洞试验%数值仿真
充水壓力容器%超高速撞擊%風洞試驗%數值倣真
충수압력용기%초고속당격%풍동시험%수치방진
pressure container filled with water%hypervelocity impact%wind tunnel test%nu-merical simulation
通过试验和数值仿真研究铝球以约2.5 km/s的速度撞击球形充水压力容器的撞击特性,容器为先充约80%的水再充2.0MPa氮气的球形不锈钢压力容器。结果表明:超高速撞击充水压力容器的主要损伤为穿孔和爆裂;铝球撞击穿透容器后在水中减速明显,未对容器后壁造成明显损伤;压力容器的工作压力相同时,在相近的撞击参数下,设计压力小的压力容器更易发生爆裂。研究结果可为在轨航天器上的压力容器设计和空间碎片防护提供参考。
通過試驗和數值倣真研究鋁毬以約2.5 km/s的速度撞擊毬形充水壓力容器的撞擊特性,容器為先充約80%的水再充2.0MPa氮氣的毬形不鏽鋼壓力容器。結果錶明:超高速撞擊充水壓力容器的主要損傷為穿孔和爆裂;鋁毬撞擊穿透容器後在水中減速明顯,未對容器後壁造成明顯損傷;壓力容器的工作壓力相同時,在相近的撞擊參數下,設計壓力小的壓力容器更易髮生爆裂。研究結果可為在軌航天器上的壓力容器設計和空間碎片防護提供參攷。
통과시험화수치방진연구려구이약2.5 km/s적속도당격구형충수압력용기적당격특성,용기위선충약80%적수재충2.0MPa담기적구형불수강압력용기。결과표명:초고속당격충수압력용기적주요손상위천공화폭렬;려구당격천투용기후재수중감속명현,미대용기후벽조성명현손상;압력용기적공작압력상동시,재상근적당격삼수하,설계압력소적압력용기경역발생폭렬。연구결과가위재궤항천기상적압력용기설계화공간쇄편방호제공삼고。
In order to study the characteristic of pressure container impacted by space debris, the characteristics of pressure container filled with water under hypervelocity impact were studied by test and simulation.The targets were ball pressure containers welded by stainless steel and were charged with water occupying about 80% volume of container and nitrogen of 2.0MPa be-fore test.The water was used to simulate liquid in the pressure container of spacecraft,and the nitrogen of 2.0MPa was used to simulate the work pressure of container.The projectiles were a-luminum spheres,and the impact velocities were about 2.5km/s.The damage models of ball pressure container were obtained by test,the moving characteristic of aluminum sphere in water was simulated.The results showed that the main damage were perforation and burst for ball pressure container filled with water under hypervelocity impact.The fragments generated by pro-j ectile impacting pressure container were decelerated evidently by the water in container which caused no evident damage on the back wall of pressure container.Under the same working pres-sure,the pressure container with low designing pressure would burst more possibly.The study conclusions provided reference for designing and protection from space debris of pressure contain-er of on-orbit spacecraft.