| 1. | This deduction forms the basis of the two-temperature postulate for composite propellant combustion .
这种推理就是构成复合推进剂燃烧中两温概念的基础。 |
| 2. | Liquid propellant combustion processes are quite complicated and defy precise analytical description .
液体推进剂燃烧过程是相当复杂的，很难对其进行严谨的分析描述。 |
| 3. | Measurement of small - signal gain on solid propellant combustion driven co2 gasdynamic laser
2气动激光小信号增益测量 |
| 4. | The results show that the thermodynamic properties of propellant combustion gas products have an important effect on its expanding power , and the correlation between conventional energy parameters such as impetus , potential energy and its power capability is not identical
结果表明，发射药燃气产物的热力学性质对其膨胀做功具有较大的影响，传统的火药力或潜能能量参数与做功能力之间的关系并非完全一致。 |
| 5. | In order to evaluate energy parameters of propellant accurately and impersonally , thermodynamic parameters of different propellant formulations were computed by potential energy method , and the correlations between the thermodynamic parameters and expanding power capability of propellant combustion gas in barrel weapon were researched
摘要为了更加准确和客观地评价发射药的能量参数，采用内能法计算了不同组分发射药配方的热力学参数，研究了发射药燃烧气体在身管武器中的膨胀做功能力与热力学参数的相互关系。 |
| 6. | The coating processes and quality checking methods for low temperature coefficient coated high - energy nitroamine propellant have been studied based on the experiment data treatment and comparison of ltsc propellant combustion properties in closed vessel with that in gun , we found that there are some combustion functions in closed vess el are similar to that in gun
通过对低温感硝胺火药在密闭爆发器和火炮膛内实验数据的处理与比较，找出了其在爆发器和火炮膛内燃烧特征相似的一些函数关系式，为利用密闭爆发器试验模拟火炮弹道性能提供了基础。 |
