航空学报 > 2007, Vol. 28 Issue (4): 827-832

基于遗传算法和空间推进方法的单壁扩张喷管优化设计研究

陈兵,徐旭,蔡国飙   

  1. 北京航空航天大学 宇航学院
  • 收稿日期:2006-05-17 修回日期:2006-12-26 出版日期:2007-07-10 发布日期:2007-07-10
  • 通讯作者: 陈兵

Optimization Design of Single-expansion-ramp Nozzles Using Genetic Algorithms-Based on a Parabolized Navier-Stokes Solver

CHEN Bing,XU Xu,CAI Guo-biao   

  1. School of Astronautics, Beijing University of Aeronautics and Astronautics
  • Received:2006-05-17 Revised:2006-12-26 Online:2007-07-10 Published:2007-07-10
  • Contact: CHEN Bing

摘要:

将单目标遗传算法和多目标遗传算法(包括NSGA-II和NCGA),与高效、高精度的空间推进流场数值模拟方法——SSPNS方法相结合,对二维超燃冲压发动机尾喷管即单壁扩张喷管(SERN)进行了气动优化设计研究。在巡航点(Ma=6.0)讨论了推力系数CT最大单目标模型,推力系数CT最大升力系数CL最大两目标模型,以及推力系数CT最大升力系数CL最大俯仰力矩系数Cm最小三目标模型,分别得到了喷管的最大推力设计和关于多个目标性能的Pareto最优前沿。结果表明,扩张壁初始扩张角θr,i和外罩长度Lc对CT影响较大;较小的Lc和较大的θr,i设计,将降低外罩内表面的负升力作用而使得SERN的CL较大;较长外罩和较小的θr,i,对应Pareto最优设计的CM较小。

关键词: 单壁扩张喷管, 优化设计, 遗传算法, 空间推进算法, Pareto最优前沿

Abstract:

The single- and multi-objective optimization designs of several 2D single-expansion-ramp nozzles (SERNs) are carried out by single-objective genetic algorithm (GA) and multi-objective GAs (including NCGA and NSGA-II). In these optimization design processes, the SERN flowfields are calculated with SSPNS (single-sweep Parabolized Navier-Stokes algorithm) codes which are proved highly accurate and highly efficient for supersonic/hypersonic flowfield simulations. The single-objective optimization design results show that the objective (i.e. thrust coefficient) is improved, but the lift coefficient is too low.

Key words: single-expansion-ramp , nozzle , (SERN),  , optimization , design,  , genetic , algorithms , (GAs),  , spacemarching , algorithms,  , Pareto , optimum , front

中图分类号: