Detonation is a secondary explosion that occurs in the combustion chamber after the spark jumps the sparkplug gap . 爆震是在燃烧室内当火花跳过火花塞电极间隙以后发生的一种二次爆燃。
The location of the instability zones is dictated by the combustor geometry and the steady-state combustion characteristics . 不稳定性区域的位置取决于燃烧室几何特性和稳定燃烧特性。
One study used an eight-foot diameter toroidal combustor, burning liquid oxygen and gaseous hydrogen, with four different injectors . 有一项研究采用8英尺直径的环形燃烧室用四种不同的喷注器，推进剂是液氧和气氢。
To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood . 为了分析液体推进剂火箭发动机燃烧室中存在的非稳态环境，必须很好地了解稳态状态。
When liquid propellants are used the fuel and oxidize are fed under pressure to one or more combustion chambers and expanded to atmosphere through convergent-divergent nozzles . 当使用液体推进剂时，在压力作用下，燃料和氧化剂输送到一个或几个燃烧室中，并通过收敛-打散喷管，排到大气中。
Large eddy simulation of vortex shedding for model srm 模型燃烧室紊流燃烧的大涡模拟
Lean diffusion combustion mechanism in bump combustion chamber 燃烧室的稀扩散燃烧机理
Electrical connectors between burner and heat generator 燃烧室和发热器之间的电气连接器
Study on primary combustion zone of aeroengine combustor 航空发动机燃烧室主燃区特性的研究
