as the air-breathing engine, the performance of solid rocket ramjet is determined not only by structure of engine and the performance of propellant, but also by flight condition.
作为吸气式发动机,其性能不仅取决于发动机本身结构和推进剂性能,与飞行状态也有密切的联系。
by means of block structure grid and second-order zonal solver method, the research on supersonic inlet performance of solid rocket ramjet assisted range projectiles was carried out.
the numerical simulation of supersonic inlet internal turbulent flow of solid rocket ramjet assisted range projectiles was performed by 2-order implicit tvd.
应用二阶隐式tvd格式对固体火箭沖压发动机增程弹丸超音速进气道内部湍流流场进行了数值仿真。
numerical calculation model and method are applicable to analyzing reacting flow field of the solid rocket ramjet with central air-inlet mode.
采用的数值计算模型和方法适用于分析中心进气式固沖发动机反应流场。
physical and mathematic model of investigating combustion characteristics of secondary combustion chamber for static extended solid rocket ramjet was established.
首先建立研究静止增程固体火箭沖压发动机补燃室燃烧特性的物理和数学模型。
the paper presents the composition, functions, technical performance and research of the solid rocket ramjet engine ground test equipment and measurement control system in detail.
介绍了固体火箭沖压发动机地面实验装置及测控系统组成、功能、技术指标和可以开展的研究工作。
thrust regulation is a key technology on the solid liquid rocket ramjet engine.
推力调节是整体式固液火箭沖压发动机研究的一项关键技术。
the numerical simulation of turbulent combustion in the afterburner of solid rocket ramjet was performed by applying the probability density function non -premixed mode.