机译:不同间隙几何形状配置对高负荷压缩机级联中空气动力学性能的影响
Energy Science and Engineering School, Harbin Institute of Technology, Harbin, Heilongjiang, China,Engine Aerodynamic Research Center, Energy Science and Engineering School, Harbin Institute of Technology, Harbin, 150001, China;
Energy Science and Engineering School, Harbin Institute of Technology, Harbin, Heilongjiang, China;
Energy Science and Engineering School, Harbin Institute of Technology, Harbin, Heilongjiang, China;
Energy Science and Engineering School, Harbin Institute of Technology, Harbin, Heilongjiang, China;
Aerospace propulsion system; compressor blade; variable stator vane; clearance; flow characteristic;
机译:尖端几何形状和尖端间隙对线性压缩机级联空气动力学性能的影响
机译:改进的微涡发生器对高负荷压缩机叶栅空气动力学性能的影响
机译:轴向不均匀尖端间隙对压缩机叶栅气动性能影响的实验研究
机译:轴流压气机叶片设计可降低空气动力性能并保持叶尖间隙的稳定性。
机译:加压定量吸入器气雾剂的空气动力学粒度分析:安徒生8级级联撞击器下一代药物撞击器和3321型空气动力学粒度仪气溶胶光谱仪的比较
机译:尖端几何形状和尖端间隙对线性压缩机级联空气动力学性能的影响
机译:壁面旋转对叶尖间隙高速压缩机叶栅性能的影响