机译:带有壳体凹槽和尖端注入的跨音速轴向压缩机的空气动力学优化
Department of Mechanical Engineering, Inha University, Incheon, Republic of Korea;
Department of Mechanical Engineering, Inha University, Incheon, Republic of Korea;
Department of Mechanical Engineering, Inha University, 253 Yonghyun-Dong, Nam-Gu, Incheon 402-751, Republic of Korea;
Axial compressor; casing groove; injection; Reynolds-averaged Navier-Stokes equations; stall margin; adiabatic efficiency;
机译:带有壳体凹槽的超音速轴向压缩机的气动性能与叶尖的注射和弹出结合
机译:带有壳体凹槽的跨音速轴向压缩机的空气动力学分析和优化,以提高运行稳定性
机译:带有套管凹槽并结合注射的轴流压气机的气动性能
机译:套管槽槽轴压缩机空气动力学性能的参数研究及尖端注入
机译:跨音速轴向压缩机中叶尖间隙流与周向槽套管处理的相互作用
机译:跨音速下高度不规则物体的空气动力学— STRATOS飞行数据分析
机译:单个和多周向套管槽,用于跨音轴压缩机的失速缘改善