Heat transfer possibly results in the thermal wrinkling of transpiration cooling platelet of the liquid rocket engine (LRE) 's thrust chamber.
液体火箭发动机发汗冷却推力室的结构层板可能出现受热皱损。
Two-phase turbulent reacting flow model of the internal operating processes in Liquid Rocket Engine (LRE) is set up in non-orthogonal curvilinear coordinates.
建立了任意斜交曲线坐标系下液体火箭发动机(LRE)内部工作过程的气液两相湍流化学反应流模型。
The leak of Liquid Rocket Engine (LRE) is very common and dangerous.
火箭发动机的泄漏是常见和极其危险的故障。
The leak of Liquid Rocket Engine (LRE) is very common and dangerous.
火箭发动机的泄漏是常见和极其危险的故障。
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