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Modelling Tone Propagation from Turbofan Inlets - The Effect of Extended Lip Liners

机译：涡轮机入口的模拟音调传播 - 延长唇线鞋的效果

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《American Institute of Aeronautics and Astronautics/Corporate Emergency Access System Aeroacoustics Conference Exhibit》|2002年||共11页
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1. Acoustic scattering by an axially-segmented turbofan inlet duct liner at supersonic fan speeds [J] . McAlpine A, Astley R, Hii VJT, Journal of Sound and Vibration . 2006,第4a5期

机译：轴向分段涡轮风扇进气管道衬里在超音速风扇速度下的声散射
2. Acoustic scattering by a spliced turbofan inlet duct liner at supersonic fan speeds [J] . McAlpine A, Wright MCM Journal of Sound and Vibration . 2006,第3a5期

机译：超音速风扇转速下涡轮风扇进气道衬管的接合处的声散射
3. Propagation and Decay of Shock Waves in Turbofan Engine Inlets [J] . Dilip Prasad, Jinzhang Feng Journal of turbomachinery . 2005,第1期

机译：涡扇发动机进气道中冲击波的传播和衰减
4. Modelling Tone Propagation from Turbofan Inlets - The Effect of Extended Lip Liners [C] . R. Astley, J. Hamilton, N. Baker, 8th AIAA/CEAS Aeroacoustics Conference amp; Exhibit . 2002

机译：模拟涡轮风扇进气口的音调传播-扩展唇线笔的效果
5. The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets [D] . Cleary, Spencer. 2018

机译：高旁路比率涡发发动机与固定锥形尖峰入口的超音速性能
6. Comparative modelling of crack propagation in elastic–plastic materials using the meshfree local radial basis point interpolation method and eXtended finite-element method [O] . Yazhe Li, Nengxiong Xu, Jinzhi Tu, 2019

机译：使用无网格局部径向基点插值法和扩展有限元法对弹塑性材料中裂纹扩展进行比较建模
7. Modeling of Inlet Distortion using a Combined Turbofan and Nacelle Inlet Model during Crosswind and Low Speed Forward Operation [O] . Kiran Vunnam, Robert Hoover 2015

机译：在侧风和低速前进操作中使用组合涡轮风扇和机舱进气道模型的进气道变形
8. Investigation at transonic speeds of the effects of inlet-lip sweep on the internal-flow characteristics of a semielliptical air inlet with an inlet-lip stagger of 30 degrees [R] . Trescot, Charles D , Jr 1957

机译：进口唇扫描对半椭圆形进气口内部流动特性的跨音速速度的研究，进口唇口错开30度

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