...
机译:小翼在发动机代表马赫数和雷诺数下的空气热性能
Department of Engineering Science, University of Oxford, Parks Road, Oxford, 0X1 3PJ, United Kingdom;
Department of Engineering Science, University of Oxford, Parks Road, Oxford, 0X1 3PJ, United Kingdom;
Department of Engineering Science, University of Oxford, Parks Road, Oxford, 0X1 3PJ, United Kingdom;
Department of Engineering Science, University of Oxford, Parks Road, Oxford, 0X1 3PJ, United Kingdom;
Department of Engineering Science, University of Oxford, Parks Road, Oxford, 0X1 3PJ, United Kingdom;
Rolls-Royce PLC, Turbine Systems (FH-3), Bristol, BS34 7QE, United Kingdom;
Rolls-Royce PLC, Turbine Systems, P.O Box31, Derby, DE24 8BJ, United Kingdom;
cctv: closed circuit television; c_x: axial chord; gap: distance between blade tip and casing endwallgutter = groove extending from leading edge to trailing; edge along the camber line; hp: high-pressure; hslc: high speed linear cascade;
机译:发动机代表马赫数和雷诺数下的冷却小翼的空气热性能
机译:用于改善高压涡轮机热性能的小翼
机译:高压涡轮叶栅中冷却的小翼梢的空气热性能
机译:发动机代表航迹和雷诺数下的冷却小翼的空气热性能
机译:在发动机代表马赫数中,在中等至低雷诺数的事件耐高压涡轮机叶片的空气动力学损失的实验研究
机译:MACH模型:从能力到公共卫生从业人员的指导和绩效
机译:Mach 5组合循环引擎的Ramburner扇区的排放性能
机译:对于各种雷诺数,攻角和鼻子形状,以6.7马赫的12.5%锥体进行空气测试