固体火箭技术2015，Vol.38Issue(6)：827-832,6.DOI:10.7673/j.issn.1006-2793.2015.06.014
HTPB复合固体推进剂粘弹性应变能及非线性本构模型
Viscoelastic strain energy and nonlinear constitutive model for HTPB composite solid propellant
摘要
关键词
HTPB推进剂/应变能/非线性回归/参数函数/本构方程/变形Key words
HTPB propellant/strain energy/nonlinear regression/parametric function/constitutive equation/deformation引用本文复制引用
张晓,郑坚,彭威,张前图..HTPB复合固体推进剂粘弹性应变能及非线性本构模型[J].固体火箭技术,2015,38(6):827-832,6.
