用于静力分析的航空结构分析系统是航空工业首次研制的一个大型程序系统。
This aeronautical structural analysis system for static analysis(H AJIF-I) is the first large software system developed by the Chinese Aeronautical Establishment(CAE).
这一系统采用多级子结构分析技术，可以适应各种类型航空结构的线性静力分析。
By using multilevel substructure analysis and finite element displacement method, this system is suitable for various linear static analysis of aeronautical structures.
结合现有的转子结构动力特性计算方法，开发出分析航空发动机转子系统动力特性的通用计算程序。
According to the calculating methods of current rotor structure dynamic characteristics, a general calculating program of analyzing aero-engine rotor system is developed.
在详细分析了军事航空监视的系统结构和工作流程的基础上，设计了真实飞行搭载试验的演示验证方案并进行了相关试验。
On the basis of the system architecture and working flow of military aviation surveillance, a verifying solution is planned and associated experimentation is conducted on a real carrying flight.
综合通用航空总线测试系统的特点和体系结构，实现了通用航空总线实时测试与分析平台。
Synthesize in the characteristics and system structure of universal avionics bus test system, carry out the platform of universal avionics bus real-time test and analysis.
着重探讨和分析了国外最新一代军、民用飞机上使用的航空电子系统体系结构——综合模块化航空电子系统(IMA)。
The latest generation of avionics architecture, namely Integrated Modular architecture (IMA) used in the foreign military and civil aircraft is especially discussed and analyzed in this paper.
是中国航空研究院领导研制的航空结构动力分析系统。
HAJIF-II is a program system developed by Chinese Aeronautical Establishment(CAE).
是中国航空研究院领导研制的航空结构动力分析系统。
HAJIF-II is a program system developed by Chinese Aeronautical Establishment(CAE).
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