机译:线性级联中具有各种膜孔配置的刮板末端的膜冷却效果研究
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
Blade tip; Film-hole arrangement; Cooling effectiveness; Experimental test; Linear cascade wind;
机译:吸气侧压条尖端对线性振荡压缩机叶栅气动弹性稳定性影响的实验研究
机译:线性叶栅中不同吹扫槽配置的涡轮叶片端壁膜冷却效率
机译:相位匹配配置中多级(chi)〜((2))级联的非线性相移的解析研究
机译:线性级联中不同吹气槽构型的涡轮叶片端壁膜冷却效率
机译:级联组态工业过程的非线性自适应控制及其在造纸真空脱水过程中的应用。
机译:液滴接口双层网络的微流体生成结合了线性和非线性配置中的实时尺寸分类
机译:线性级联中HP涡轮叶片的局部和腔型耳钉尖端的性能
机译:线性化非定常气动分析在标准级联配置中的应用