| 1. | In - wall temperature measure of the closed - bomb
爆发器内壁温度的测试 |
| 2. | The closed bomb test is performed , and the power strength , impact sensitivity , flash point are tested
进行了密闭爆发器实验，测试了火药力、撞击感度和爆发点等性能。 |
| 3. | Furthermore , the vlwr calculated results were used to guide the designation of the combustion pot , whose measured output pressure is close to the designed output value
利用计算结果和密闭爆发器实验结果指导了燃气做功元件装药设计，实验表明输出最大压力预估值与实验值接近。 |
| 4. | Abstract : the properties of coated propellants made by n ew and old technology were studied by the ways of determining the thickness of c oating layer , experiments of termination combustion and closed bomb combustion
文摘:通过火药包覆层厚度的测定，中止燃烧及密闭爆发器试验，比较研究了新旧两种工艺制造的低温感包覆火药的性能。 |
| 5. | The measured output pressure was close to the designed value , which indicate that using the calculated value and experimental data to guide the designation of the combustion pot is reasonable and practical
实验结果表明，燃气做功元件的最大输出压力的实测值与理论设计值接近，表明采用vlwr状态方程方法和密闭爆发器实验结果指导燃气做功元件装药设计是可行的。 |
| 6. | The combustion parameters such as co - volume and impetus of the studied explosives were obtained through two methods , one is the standard closed bomb test ( cbt ) and the other is theoretic calculating with vlwr eos . the calculated values agreed well with experimental data
研究采用密闭爆发器实验对炸药的燃烧性能参数(如火药力、余容等)进行了测试，并采用vlwr状态方程方法对这些燃烧参数进行了热力学计算，获得与实验吻合的燃烧性能参数。 |
| 7. | This is the theoretical foundation for simulating the gun interior ballistic performance using the closed vessel experiment . based on the functions from closed vessel experiments , the ballistic simulation results of maximum chamber pressure , muzzle velocity and p - t curves of a 105mm gun charged with ltsc nitroamine propellant at + 50c , + 15c and - 40 environmental temperature were in good agreement with experimental data
在密闭爆发器实验的基础上，应用可视化程序对某105mm火炮采用低温感硝胺火药在+ 50 、 + 15和- 40环境温度下的最大膛压、初速以及膛压?时间曲线进行了弹道模拟，模拟与实验结果具有较好的一致性。 |
| 8. | 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。 |
| 9. | ( 2 ) calculation of the combustion parameters the combustion parameters of hmx , rdx , hns - i and b / kno _ ( 3 ) were calculated with vlwr code . the thermodynamic function of boron oxide was fitted by method of the least square to janaf thermo - chemical table , and their coefficients were determined
( 2 )炸药及点火药燃烧性能参数计算应用热力学程序vlwr计算hmx 、 rdx 、 hns -及点火药b kno _ 3的燃烧性能参数及燃烧平衡产物组成，得到了与密闭爆发器实验相近的燃烧性能参数。 |
| 10. | In this dissertation , the application of low temperature sensitivity coefficient ( ltsc ) high - energy nitroamine propellant in a 105mm gun has been studied theoretically and experimentally . the ltsc coated propellant ingredient calculation program , the closed vessel and gun experiment data processing program and the ballistic simulation program , which can simulate gun interior ballistic performances based on closed vessel experiment data , have been programmed with visual program design method
本文对低温感高能硝胺发射药在某105mm火炮上的应用进行了理论和实验研究，编写了低温感包覆火药包覆层组分计算、密闭爆发器和火炮实验数据处理以及利用密闭爆发器实验模拟火炮弹道性能等可视化应用程序。 |
