固体火箭技术
固體火箭技術
고체화전기술
JOURNAL OF SOLID ROCKET TECHNOLOGY
2014年
6期
819-823
,共5页
钮然铭%陈雄%周长省%周清春
鈕然銘%陳雄%週長省%週清春
뉴연명%진웅%주장성%주청춘
内聚力模型%推进剂/衬层%数值研究%脱粘
內聚力模型%推進劑/襯層%數值研究%脫粘
내취력모형%추진제/츤층%수치연구%탈점
cohesive zone model%propellant/insulation%numerical research%debond
为提高丁羟( HTPB)推进剂/衬层界面数值仿真结果的准确性,首先改进了单搭接试件,通过剪切实验获取界面断裂参数,而后分别采用双线型模型和指数型模型对试件进行数值研究,进行影响分析,并在此基础上建立了一种基于损伤变量的自定义内聚力模型,使模型具有了明确的物理含义。结果表明,改进的单搭接试件能够测定柔韧粘接件的II型断裂参数;II型界面断裂时,内聚力曲线形式与实验曲线形式一致;该基于损伤的内聚力模型能够比双线性模型和指数型模型更准确地反映HTPB推进剂/衬层界面的II型断裂性质。
為提高丁羥( HTPB)推進劑/襯層界麵數值倣真結果的準確性,首先改進瞭單搭接試件,通過剪切實驗穫取界麵斷裂參數,而後分彆採用雙線型模型和指數型模型對試件進行數值研究,進行影響分析,併在此基礎上建立瞭一種基于損傷變量的自定義內聚力模型,使模型具有瞭明確的物理含義。結果錶明,改進的單搭接試件能夠測定柔韌粘接件的II型斷裂參數;II型界麵斷裂時,內聚力麯線形式與實驗麯線形式一緻;該基于損傷的內聚力模型能夠比雙線性模型和指數型模型更準確地反映HTPB推進劑/襯層界麵的II型斷裂性質。
위제고정간( HTPB)추진제/츤층계면수치방진결과적준학성,수선개진료단탑접시건,통과전절실험획취계면단렬삼수,이후분별채용쌍선형모형화지수형모형대시건진행수치연구,진행영향분석,병재차기출상건립료일충기우손상변량적자정의내취력모형,사모형구유료명학적물리함의。결과표명,개진적단탑접시건능구측정유인점접건적II형단렬삼수;II형계면단렬시,내취력곡선형식여실험곡선형식일치;해기우손상적내취력모형능구비쌍선성모형화지수형모형경준학지반영HTPB추진제/츤층계면적II형단렬성질。
In order to raise the precision of the numerical simulation result of HTPB propellant/insulation,firstly,the SLJ test was improved and conducted to obtain the interface parameters. Then the bilinear CZM and the exponential CZM were adopted to conduct the numerical analysis,separately.At last,an influence analysis was made and a customized CZM model was built base on damage variable,which gave the model a significant physical meaning.The result shows that the improved SLJ test can determine the interface parameters of ductile adherends.The CZM law has a similar trend to the simulation curve,and the CZM based on damage can better simulate mode?II interface fracture properties between HTPB propellant and insulation than bilinear CZM and exponential CZM.