摘要
The influence of pressure gauges to the reaction flow field is studied experimentally. Pressure histories during the shock initiation process for a modified double based propellant is measured with enhanced accuracy. A new reaction rate equation for modified double based propellant is proposed, and the coefficients in the equation are calibrated on the basis of a global calibration method. The shock initiation process is also simulated for the propellant, and the results show that the calculation agrees well with the measured histories.
源语言 | 英语 |
---|---|
页(从-至) | 443-448 |
页数 | 6 |
期刊 | Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology |
卷 | 14 |
期 | 4 |
出版状态 | 已出版 - 1994 |