| 引用本文: | Shen Huairong..[J].国防科技大学学报,1995,17(3):109-113.[点击复制] |
| Shen Huairong.THE CREEP-DAMAGE MODELING CORRELATED TO TEMPERATURE FOR COMPOSITE SOLID PROPELLANT[J].Journal of National University of Defense Technology,1995,17(3):109-113[点击复制] |
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| 投稿日期：1994-07-02 |
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| THE CREEP-DAMAGE MODELING CORRELATED TO TEMPERATURE FOR COMPOSITE SOLID PROPELLANT |
| Shen Huairong1 |
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(Department of Aerospace Technology，108 Laboratory，NUDT，Changsha，410073)
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| Abstract: |
| The creep-damage modeling correlated to temperature has been described for a kind of composite solid propellant (CSP) in this paper. The material parameters of the modeling were determined by creep experiments of uniaxial and biaxial loading. The modeling is useful for analysis of solid rocket motor and for prediction of service life of the CSP. |
| Keywords: composite solid propellant,creep damage,temperature |
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