面积律可控/无控的环形隔离段优化设计对比OA
Optimization Design Comparison of Area Law Controlled/Uncontrolled Annular Isolator
以高超声速冲压发动机环形隔离段为对象,提出基于B样条的面积律(沿程截面积变化规律)可控/无控隔离段参数化建模方法,并开展面积律可控/无控隔离段气动优化研究.结果表明:环形隔离段壁面形状对出口气流品质影响显著,型面转弯先急后缓和先缓后急均易在管道内形成大规模分离区,造成出口总压恢复系数下降;而缓急相当的构型无明显流动分离,总压恢复性能较优.隔离段出口总压恢复性能和抗反压性能的最优方向并不一致,面积律无控条件下最优隔离段总压恢复系数达到0.778,但其仅能抵抗172倍自由来流反压,面积律可控条件下的最优隔离段总压恢复系数为0.764,其抗反压能力达到196倍自由来流反压.鉴于面积律可控隔离段最优构型在总压恢复降低仅1.82%的情况下,抗反压能力提升了13.95%,为兼顾隔离段总压恢复和抗反压能力,建议后续可采用面积律可控方式对隔离段进行设计.
A parametrized modeling method based on B-Splines for area law(law of variation of cross section area along the path)controlled/uncontrolled annular isolator is proposed,and aerodynamic optimization of the area law controlled/uncontrolled isolator is undertook by using the aerodynamic optimization method.The results indicate that the wall con-figuration of annular isolator has significant effect on exit flow quality,the profile turns rapidly then gradually and the one turns gradually then rapidly all tend to form large-scale separated flows which cause a decrease in the total pressure recovery coefficient.However,there is no obvious separation for the flow in the configuration with equal urgency and the total pressure recovery performance is better.The optimal directions of total pressure recovery performance and back-pressure resistance performance of the isolator are not consistent,total pressure recovery coefficient of optimal iso-lator under area law uncontrolled condition reaches 0.778,but it can only resist 172 times the pressure of the free stream,total pressure recovery coefficient of optimal isolator under area law controlled condition reaches 0.764 and it can resist 196 times the pressure of the free stream.In view of the total pressure recovery coefficient of the optimal area law controlled isolator reduced only 1.82%,the back-pressure resistance ability is improved by 13.95%,in order to bal-ance the total pressure recovery and the back-pressure resistance ability of the isolator,it is recommended to design the isolator in the area law controlled way.
韩云龙;徐尚成;王翼;彭思怡
国防科技大学,湖南 长沙 410073国防科技大学,湖南 长沙 410073国防科技大学,湖南 长沙 410073国防科技大学,湖南 长沙 410073
航空航天
环形隔离段B样条总压恢复系数抗反压
annular isolatorB-splinestotal pressure recovery coefficientback-pressure resistance
《海军航空大学学报》 2026 (2)
315-327,13
国家自然科学基金(12372298)
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