Some XSLT elements contain a sequence constructor, as can an LRE.

一些XSLT元素像LRE一样可以包含顺序构造器。

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。

If they are defined on an LRE, then they are copied to the result tree.

如果定义在LRE上则被复制到结果树中。

A namespaced attribute on an LRE must always be copied through to the result, except for those in the XSLT namespace.

LRE上带有名称空间的属性必须被复制到结果中，除非是XSLT的名称空间。

The data mining methods possibly applicable to different topics in the fault detection and diagnosis of LRE are compared.

对在液体火箭发动机故障检测和诊断的不同问题中可能应用的数据挖掘方法进行了分析比较。

The results show that the method can detect the faults occurred in the steady-state process of LRE efficiently and accurately.

试车数据验证结果表明，该方法能及时、准确、有效地检测发动机稳态过程的故障。

This paper mainly focuses on CAD of LRE design, and present studies on CAD technique of recycled cooling LRE combustion chamber.

本文的主要工作面向液体火箭发动机设计CAD技术，并选择再生冷却式液体火箭发动机推力室设计CAD技术研究作为方向。

Then, with the help of historical data from LRE test as well as real-time data from rotor test platform, the TP-FDS was validated.

通过转子试验平台实时数据和液体火箭发动机历史试车数据，验证了TP-FDS。

Lacking of fault samples is a knotty problem in the fault detection of complex systems such as Liquid-propellant Rocket Engines (LRE).

在对类似于液体火箭发动机这种复杂系统的故障检测过程中，一个非常棘手的问题是缺乏故障类样本。

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。

This paper explains the main idea in design thinking of LRE/CAA, introduces, software blocks and their function, and illustrates how to deal with some problems in software realizing process.

本文阐述了软件LRE/CAA的设计思想，介绍了软件所包括的模块和各个模块的功能，并说明了在软件实现过程中一些问题的处理方法。