乘波器的参数化设计研究  

Parametric waveriders design method study

作　　者：张杰[1] 王发民[1] 

机构地区：[1]中国科学院力学研究所高温气体动力学重点实验室,北京100080

出　　处：《空气动力学学报》2008年第1期115-118,130,共5页Acta Aerodynamica Sinica

基　　金：国家自然科学基金资助项目(90405012)

摘　　要：开展变楔角参数化乘波器的研究。研究中考虑了粘性效应,分析了不同设计参数对乘波器气动性能的影响。对比MAXWARP乘波器设计结果和数值求解NS方程的结果,验证了变楔角参数化乘波器设计方法的正确性。分析了不同的设计参数对乘波器气动性能的影响,为研究复杂的乘波器设计和优化规律提供了一个途径。参数化乘波器设计可方便的控制乘波器的外形尺寸,使乘波器的应用性大大提高。In this paper, the parametric waveriders designed with variable wedge angle is being studied. During the design process, viscous effect is being considered, and the effect of change design parametric to aerodynamic is being analysis too. Via validate with MAXWARP waveriders generate programmer and NS equation numerical simulation, it demonstrates that the parametric waveriders design method is fulfill. With the parametric analysis the design parametric effect to aerodynamic, it leads a way to understand more complex waveriders design and optimization. Because parametric waveriders design method can control the configure of result waveriders more easily, it makes parametric waveriders design more close to application.

关 键 词：乘波器 变楔角 气动性能 参数化设计 

分 类 号：V211.3[航空宇航科学与技术—航空宇航推进理论与工程] V221.3