航天器环境工程
航天器環境工程
항천기배경공정
SPACECRAFT ENVIRONMENT ENGINEERING
2012年
2期
129-133
,共5页
冲击波%峰值超压%数值模拟%液体推进剂
遲擊波%峰值超壓%數值模擬%液體推進劑
충격파%봉치초압%수치모의%액체추진제
shock wave%peak overpressure%numerical simulation%liquid propellant
针对现有液体推进剂爆炸实验危险性高、耗费大以及实验条件严格及重复性差等缺点及难点,利用Autodyn软件分别对一维和二维两种情况下液体推进剂爆炸产生的冲击波进行数值模拟,并与经验预测及相关实验研究进行比较分析。研究结果表明:在距离大于10
針對現有液體推進劑爆炸實驗危險性高、耗費大以及實驗條件嚴格及重複性差等缺點及難點,利用Autodyn軟件分彆對一維和二維兩種情況下液體推進劑爆炸產生的遲擊波進行數值模擬,併與經驗預測及相關實驗研究進行比較分析。研究結果錶明:在距離大于10
침대현유액체추진제폭작실험위험성고、모비대이급실험조건엄격급중복성차등결점급난점,이용Autodyn연건분별대일유화이유량충정황하액체추진제폭작산생적충격파진행수치모의,병여경험예측급상관실험연구진행비교분석。연구결과표명:재거리대우10
The traditional experimental study of the explosion with liquid propellant explosion is difficult, therefore, simulation studies are necessary. By using the Autodyn software, the shock waves generated by the explosion of liquid propellant in the air with liquid propellant are simulated in one-dimensional and two-dimensional cases, respectively. The results are compared with those obtained from the empirical formula and the experimental studies, with good agreement.. Not only can the peak overpressure be obtained accurately, but also the attenuation process can be made clear. The simulations thus play a significant role for the safety protection and the damage assessment for liquid propellant explosions.