A modified sweep method with decoupled leading edge and throat line for a highly loaded fan stage一种具有解耦前缘和喉线的高载荷风扇级改进扫描方法Aerospace Science and TechnologyIF5.82026-09-110PRE
Shock-dominated flow structures at the design condition of a supersonic through-flow fanPHYSICS OF FLUIDSIF4.32025-02-140PRE
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