TY - JOUR
T1 - 考虑围压效应的N15固体推进剂本构模型
AU - Zhang, Jiye
AU - Xu, Jinsheng
AU - Han, Feng
AU - Wang, Shixin
N1 - Publisher Copyright:
© 2021, Editorial Department of Journal of Aerospace Power. All right reserved.
PY - 2021/6
Y1 - 2021/6
N2 - Mechanical properties of N15 solid propellant under different confining pressures were obtained by using the confining pressure test system. Result showed that the initial modulus of the propellant did not change with the confining pressure, but the maximum tensile strength, rupture strength, the maximum elongation and elongation at break increased with the increase of confining pressure; combined with propellant's mesoscopic structure and cross section analysis, the mechanical mechanism of confining pressure effect on the propellant was revealed preliminarily; as a result of the existence of confining pressure, the particle dewetting inside the propellant was reduced, the holes' propagation delayed due to the pressure, and its crack extension and germination was inhibited, which proved that the confining pressure had strengthening effect for propellant; according to the elastic-viscoelastic correspondence principle, a constitutive model considering the confining pressure effect was established for N15 propellant. The results showed that accuracy of the constitutive model was good, and it can describe the influence of confining pressure on the mechanical properties of N15 propellant accurately.
AB - Mechanical properties of N15 solid propellant under different confining pressures were obtained by using the confining pressure test system. Result showed that the initial modulus of the propellant did not change with the confining pressure, but the maximum tensile strength, rupture strength, the maximum elongation and elongation at break increased with the increase of confining pressure; combined with propellant's mesoscopic structure and cross section analysis, the mechanical mechanism of confining pressure effect on the propellant was revealed preliminarily; as a result of the existence of confining pressure, the particle dewetting inside the propellant was reduced, the holes' propagation delayed due to the pressure, and its crack extension and germination was inhibited, which proved that the confining pressure had strengthening effect for propellant; according to the elastic-viscoelastic correspondence principle, a constitutive model considering the confining pressure effect was established for N15 propellant. The results showed that accuracy of the constitutive model was good, and it can describe the influence of confining pressure on the mechanical properties of N15 propellant accurately.
KW - Confining pressure environment
KW - Confining pressure test system
KW - Constitutive model
KW - Mechanical properties
KW - N15 propellant
UR - http://www.scopus.com/inward/record.url?scp=85110408027&partnerID=8YFLogxK
U2 - 10.13224/j.cnki.jasp.2021.06.022
DO - 10.13224/j.cnki.jasp.2021.06.022
M3 - 文章
AN - SCOPUS:85110408027
SN - 1000-8055
VL - 36
SP - 1335
EP - 1344
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 6
ER -