The effect of combustion conditions on burning-out time and maximum burning rate is researched.

调查了燃烧条件对燃尽时间和最大燃烧速率的影响。

In other circumstances, a reduced burning rate may be sought after.

在其他情况下，减少了燃烧率可要求后。

For the propellant mechanism of increasing burning rate is discussed.

分析了这种推进剂能提高燃速的机理。

Closed burner method is used for determining burning rate of the solid propellants.

密闭燃烧器法是一种间接测定固体推进剂燃速的方法。

In the alternate approach, the burning rate is expressed as a function of drop radius.

在另一种方法中，燃烧速率表示为液滴半径的函数。

The burning rate is enhanced rapidly along with the increase of Mg in the composition.

随着药剂中镁含量的提高，燃烧速度迅速增加。

A method suitable for calculating the burning rate of combustible gas in CFBC has been created.

建立了一种适合于循环流化床燃烧室(CFBC)条件下可燃气体的燃烧计算方法。

The neural network is adopted to study the burning rate identification of the solid fuel ramjet.

用神经网络技术对固体燃料冲压动机的燃速辨识问题进行了研究。

It is a reliable measuring method of the specific impulse for the high-burning rate propellants.

为高燃速推进剂比冲测试提供了可靠的试验依据。

The effect of combustion conditions on burning-out time and maximum burning rate is researched, too.

另外，燃烧温度、空气流量、升温速率和试样量影响飞灰最大燃烧速率和燃尽时间。

Twin screw extrusion technology of porous ultra high burning rate propellant (UHBRP) substitutes was studied.

研究了多孔超高燃速推进剂代料的双螺杆混合挤出工艺。

Applying burning-rate catalysts is one of optimal approaches to regulate the burning rate of HTPB propellant.

使用燃速催化剂是调节丁羟推进剂燃速的最佳途径之一。

A laser method was used for measuring transient burning rate delay of solid propellant in oscillatory combustion.

应用激光方法测量压力振荡过程中的固体推进剂瞬态燃速。

The thermal stability of high burning rate propellant is studied by DSC, methyl violet test and weight loss test.

甲基紫试验和失重试验研究了高燃速推进剂的热安定性。

The combustion of hydrogen in coke under regeneration is also discussed and its relative burning rate is reckoned.

讨论了在催化裂化再生器中焦中氢元素的燃烧，并推算出其相对燃烧速度。

The materials of tube for loading particles and the load height have less effect on the apparent mass burning rate.

装填药粒用的壳体材料和药粒装填高度对传火速度的影响不显著。

Variety of the burning rate pressure exponent will give expression to the additive's catalysis to the propellant's combustion.

燃速压力指数的变化情况说明了催化剂对燃烧所起催化作用的大小。

The approximate analytical solution on the burning rate of droplet mass is also found on the basis of some simplified hyPotheses.

在一些简化假设的基础上，找到了液滴质量燃速的近似解析解。

The homogeneity of certified reference material is studied by acoustic emission method for composite solid propellant burning rate.

采用声发射燃速测试方法研究了复合固体推进剂方坯燃速的均匀性。

A low burning rate NEPE propellant were investigated by means of adding some burning rate inhibitors and adjusting its composition.

采用调节NEPE推进剂的配方组分、添加降速剂等手段进行了一系列降低燃速的研究。

When FG and YB are incorporated, they may obviously reduce the pressure exponent of HTPB propellant as well as enhancing the burning rate.

当FG与亚铬酸铜组合使用时，可在提高推进剂燃速的同时大幅度地降低燃速压强指数。

Thus, improving the condensed-phase reaction can increase of the burning rate for fuel-rich propellant with boron in low pressure condition.

分析表明促进凝相反应有利于含硼富燃料推进剂低压燃速的提高。

The results show that polymer materials can decrease the HMX's burning rate, while bonding agents have little influence on the HMX's combustion property.

试验结果表明，聚合物材料将降低HMX的燃烧速度，而小分子键合剂对HMX燃烧性能的影响不大。

The effect of hydrogen on methane combustion and ignition temperature, burning rate and burnout time are discussed through analyzing the calculated results.

通过分析计算，讨论了氢气对甲烷燃烧过程及着火温度、燃烧速率、燃尽时间的影响。

The combustion catalyst adopted by ordinary double base propellant can adjust the burning rate. It's necessary to study further on the combustion mechanism.

该推进剂具有低特征信号、低易损性等特点，用一般双基药所采用的燃烧催化剂可调节燃速，深入研究其燃烧机理很有意义。

The results of the burning rate measurement showed that the nanometer sized lead oxide can play a role in decreasing the pressure exponent of NEPE propellant.

通过纳米氧化铅在NEPE推进剂中的实际应用效果表明：纳米氧化铅可有效的降低NEPE推进剂的燃速压力指数。

Among those methods to improve the burning rate of solid propellant, the nanometer-sized catalyst has been considered as one kind of most prospective methods.

在提高固体推进剂燃速的众多方法中，采用纳米催化剂被认为是最有前途的方法之一。

Based on the results of tests, the relationship between burning rate augmentation and burning time is discussed. A physical model is also presented and studied.

根据试验结果，论述了燃速增加率与燃烧历程的关系，提出和探讨了燃烧物理模型问题。

The results showed that the main influencing factor to the interior ballistics of solid motor with high energy propellant is the slow descending of burning rate.

结果表明，燃速缓慢下降是影响高能推进剂发动机内弹道性能变化的主要因素。

The static burning rate of cigarette is first increased, continuously come up to a "peak value", and then let up while the dosage of burning accelerant is increased.

在相同的实验条件下，卷烟的自由燃烧速度随助燃剂添加量的增加呈先增大后减小的变化规律。