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高超声速飞行器一体化构型部件的初步设计与性能评价
引用本文:郭效芝,李健.高超声速飞行器一体化构型部件的初步设计与性能评价[J].指挥控制与仿真,2013,35(5).
作者姓名:郭效芝  李健
作者单位:装备学院基础系,北京机电工程研究所
摘    要:分析了高超声速巡航飞行器机体/发动机一体化构型的特点,进行了一体化构型的部件划分。系统地研究了一体化构型各部件的设计条件、设计内容、设计要求和设计参数,提出了一体化构型各个部件的性能评价方法。论文的方法可用于高超声速巡航飞行器机体/发动机一体化构型的快速初步设计与性能评价。

关 键 词:高超声速  巡航飞行器  一体化

Preliminary Design Methods for ConstructionParts of the Integrative Configuration for Hypersonic Vehicle
guoxiaozhi and li jian.Preliminary Design Methods for ConstructionParts of the Integrative Configuration for Hypersonic Vehicle[J].Command Control & Simulation,2013,35(5).
Authors:guoxiaozhi and li jian
Institution:Department of Basic Courses, Academy of Equipment,Beijing Electromechanical Enginnering Reseach Institute
Abstract:Based on the characteristic of the integrative configuration for hypersonic cruise vehicle, construction parts of the airframe/engine integrative configuration are defined. Preliminary design methods for construction parts of the airframe/engine integrative configuration are proposed and studied systemically, and the performance assessment methods for construction parts are also presented. The methods proposed in this paper have value for hypersonic cruise vehicle preliminary design.
Keywords:hypersonic  cruise vehicle  integrative configuration
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