讨论了某型航空发动机试车计算机辅助试验系统的开发；
The development of computer aided testing system for certain aeroengine test-run is discussed.
在本文中讨论了航空发动机试车自动数据采集和处理系统的设计和实现。
In this paper, the design and the implementation of automatic data acquisition and processing system for the aeronautic engine testing are described.
根据本文所论述的方法，实现了该功能并已投入了某型航空发动机试车实验使用。
On the basis of the method present, the function is achieved and has been used for aeroengine test.
本文结合WS9发动机试车数据库，对航空发动机试车数据库的数据挖掘技术应用作了尝试性的研究。
In this paper, data mining techniques were introduced to investigate the test-driving database of WS9 aero-engines.
对采用模型参考自适应控制方法设计带有多项约束条件的航空发动机试车自动试车控制系统进行了研究。
An automatic control system of aeroengine test has been designed, based on the method of model reference adaptive control with restraints.
航空发动机试车计算机辅助试验系统中开发三分钟事件记录与回放功能可以为事后的分析提供数据依据。
The function named 3-minitue events recording and replaying in computer-aided test system for aeroengine test is able to offer data for analysis afterwards.
介绍了涡轮流量计在航空发动机试车燃油流量瞬态测量中的应用，指出了瞬态测量误差的主要来源以及测量时的注意事项。
A transient measurement method of the fuel flow using turbine flowmeter in aeroengine trial is introduced. The error sources of transient measure are also analyzed.
介绍了涡轮流量计在航空发动机试车燃油流量瞬态测量中的应用，指出了瞬态测量误差的主要来源以及测量时的注意事项。
A transient measurement method of the fuel flow using turbine flowmeter in aeroengine trial is introduced. The error sources of transient measure are a...
由于航空发动机转速高，空气流量大，排气温度高，试车时产生的强烈噪声形成大范围的环境污染；
Aerogine has the features of high rev, heavy air flux and high exhaust temperature, fierceness of noise engenders environment pollution largely during aeroengine test.
介绍了航空发动机整机试车试验流程管理系统的设计思想、功能和特点。
Design concept, function and features of the test process management system for aeroengine test were presented.
目前本系统已经用于西安航空发动机（集团）有限公司的WS9发动机的试车工作。
Now, the system has been used in WS9 engine test in Xi'an Aero Engine Company.
为此对某型航空发动机的离散试车数据点进行了多元高次多项式拟合，建立了该型号发动机的稳态特性曲线。
While the discrete test run data of an aero-engine was adapted using the high order multi-parameters polynomial fit method, the steady characteristic curves were founded.
为此对某型航空发动机的离散试车数据点进行了多元高次多项式拟合，建立了该型号发动机的稳态特性曲线。
While the discrete test run data of an aero-engine was adapted using the high order multi-parameters polynomial fit method, the steady characteristic curves were founded.
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