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simulated altitude test facility 高空模拟试车台
Indirect air heating experiment at a simulated altitude test facility 高空台间接加热试验
altitude test facility 高空试车台
An Improved Air Cooling System for Simulated Altitude Test Facilities 高空台空气降温系统的技术改造
Maintenance of Large Fuel Cooling System for Altitude Test Facilities 高空台大型燃油降温系统故障修复及调试
Bechtel designed a versatile and flexible test facility. 比奇特尔公司正在设计一套多方面的活动式的试验设备。
altitude simulation test facility 高空台
Design or set the inspection and test facilities. 设计或制定检验和测试的机制和设备；
This is a test facility that reads information from the WSDL and connects to the service directly. 这个浏览器是能从WSDL中读取信息并能直接连接到服务上的测试工具。
Hypersonic propulsion test facility is important for the scramjet ground tests. 摘要高超声速推进风洞是进行超燃冲压发动机模型地面模拟的重要试验设备。
The main parameters and advanced performance of test facilities at Yunnan high altitude EHV AC and DC test base are introduced. 阐述了云南省高海拔超高压交直流输变电试验中试基地主要设备的技术参数和先进性能。
When it becomes necessary to examine the altitude performance of an aircraft engine, three types of facilities may be used-altitude wind tunnels, altitude test beds and flying test beds. 当需要考察一台航空发动机的高空性能时，可以利用三种型式的设备，即高空风洞、高空试验台和飞行试验台。
Michael Y.Young, David A.Penz,“the design of a new turbocharger test facility,”SEA Special Publications 900176,1990. 蒋小伟、洪锜炫、熊道邦;“涡轮增压器分析与测试研究”第二十届机械工程研讨会2003.
This paper will describe the environment control system (ECS) of the test facility. 文章介绍了该模拟设备的环境控制系统。
The particularity of the altitude simulated test of an engine with Laval nozzle was analyzed in brief. The engine thrust determination and correction in altitude test with large deviation of simulated ambient pressure was put forward. 简析了拉瓦尔喷管发动机高空模拟试验的特殊性,提出了大模拟偏差条件下确定和修正拉瓦尔喷管发动机推力的方法。
According to the work and test principle of some air defense missile autopilot, an autopilot test facility is developed. 摘要根据某型防空导弹自动驾驶仪的工作原理和测试原理，研制了该驾驶仪测试设备；
Using the available data from 3 starts in simulated altitude tests,the windmilling start ignition characteristic of a turbofan engine was analyzed in this paper. 发动机点火特性+是其在极限高度与极限边界成功起动的重要影响因素。
The scramjet supersonic combustor and its test facility have been designed by enthalpy method and characteristic line method. 采用热焓法、特征线法等进行了超音燃烧室试验器的计算和设计工作。
Experimental studies of turbulent combustion were conducted in a test facility for swirl combustor with staged air injection. 本文在分级进风旋流燃烧室的实验装置上进行了湍流燃烧的实验研究。
Low temperature environment is simulated by using a cascade refrigeration system in the thermal vacuum test facility of spacecraft subassembly. 卫星部组件热真空试验设备制冷系统提供试验设备的冷黑环境。