摘要
Artificial Neural Network (ANN) theory using BP arithmetic was used to investigate the burning rate relativity of solid propellant. The result of ID model proves the feasibility and stability of this method. A two-dimension model was established. Experimental data was adopted to verify the model. The calculating results indicate the precision of predicted burning rate is higher than the 1D model. This method can be used to calculate the burning rate relativity of solid propellant.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 156-158 |
| 页数 | 3 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 25 |
| 期 | 2 |
| 出版状态 | 已出版 - 4月 2004 |
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