| 引用本文: | Cao Taiyue..[J].国防科技大学学报,1995,17(3):119-125.[点击复制] |
| Cao Taiyue.CALCULATION OF BURNING RATE CHARACTERISTICS IN ACCELERATED FIELD FOR SOME ALUMINIZED SOLID PROPELLANTS[J].Journal of National University of Defense Technology,1995,17(3):119-125[点击复制] |
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| 投稿日期：1994-06-15 |
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| CALCULATION OF BURNING RATE CHARACTERISTICS IN ACCELERATED FIELD FOR SOME ALUMINIZED SOLID PROPELLANTS |
| Cao Taiyue1 |
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(Department of Aerospace Technology，NUDT，Changsha，410073)
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| Abstract: |
| In this paper the steady state combustion model of metalized propellants in an accelerated field is used to calculate the burning rate characteristics of an aluminized HTPB propellant with two kinds of burning rate levels. A comparison between computational results and experimental results of grain slabs on a spinning test stand is made. A discussion about some problems involved in calculations is presented. |
| Keywords: aluminized propellants,accelerated field,burning rate characteristics |
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