然后，简略地证明了平衡压力的稳定条件以及燃烧室压力与平衡压力的近似关系。
The stable condition of equilibrium pressure and the approximate relationship between the chamber pressure and the equilibrium pressure are derived.
对五种不同燃烧室体积的脉冲发动机在小、中和大油门开度三种供油条件下测定其排放物。
The exhaust gas ingredients of pulse engines, with five different combustion chamber volumes, throttle valve at small, middle and wide opening positions respectively, are tested.
理论分析和试验结果均表明：燃烧室增压速率、脱粘面尺寸、边界条件等因素对脱粘面扩展均有较强的影响。
Theoretical analysis and experiment results prove that the chamber pressurization rate, the debond dimension and the boundary condition have strong effects on the propagation of the debond.
计算了燃烧室压力与初始空隙率等对燃烧过程的影响，分析了稳定燃烧时应满足的一些基本条件，结果与实验值相一致。
The effects of both chamber pressure and initial Porosity on combustion process are calculated, and some basic conditions for stable burning are analysed.
在文中所研究的引射燃烧室结构条件下，存在一个最佳二次喷管出口面积，它能使引射火箭的推力达到最大。
There exists an optimal exit area of secondary nozzle to result in a maximum thrust of rocket ejector in the light of the investigated ejector chamber structure.
本文对涡流室式柴油机在冷起动条件下主、副燃烧室内燃油喷雾和着火过程进行了高速摄影。
The high speed photography was applied to visualize the fuel spray and ignition process in main and prechamber in a swirl type diesel engine at cold starting condition.
这些相互冲突的条件要求进行折衷，但是，燃烧室设计与性能的连续改善已经导致燃烧过程“清洁”得多了。
This conflict of conditions requires a compromise to be made, but continuing improvements in combustor design and performance has led to a substantially 'cleaner' combustion process.
该系统简化后应用在定容燃烧室上，可以点燃不同初始条件下的可燃混合气。
For the simplified system was applied in a constant volume combustion chamber, the combustible mixture can be ignited at any situation.
分别对冷态条件下，无隙锥形旋流器燃烧室前扩压器内流场的分叉现象以及燃烧室内燃烧空间的流场分叉现象进行了数值模拟计算。
The numerical simulations of bifurcation phenomena in a combustor with a non slot conical swirler and in a diffuser fixed before the non slot conical swirler have been carried out.
在台阶高度一定的条件下，单台阶结构的燃烧室具有更好的燃烧性能。
Furthermore, as the total step height is the same, the combustor configuration with one backwind step has higher performance than the combustor configuration with two backwind step.
推导了引射器和燃烧室特性方程，给出了最佳结构条件的计算公式；
The characteristic equations, the optimum equations of injector and burner house are given and analyzed.
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。
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。
A method suitable for calculating the burning rate of combustible gas in CFBC has been created.
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