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Investigation of the effect of turbulence intensity and nozzle exit boundary layer thickness on stability pattern of subsonic jet

机译：湍流强度和喷嘴出口边界层厚度对亚音速射流稳定模式的影响研究

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Siavash Gohardehi; Saeed Arablu; Hossein Afshin; Bijan Farhanieh;
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1. Investigation of the effect of turbulence intensity and nozzle exit boundary layer thickness on stability pattern of subsonic jet [J] . Gohardehi Siavash, Arablu Saeed, Afshin Hossein, Mechanics & Industry . 2019,第1期

机译：湍流强度和喷嘴出口边界层厚度对亚旋转射流稳定模式的影响研究
2. Identification of the effects of the nozzle-exit boundary-layer thickness and its corresponding Reynolds number in initially highly disturbed subsonic jets [J] . Bogey C., Marsden O. Physics of fluids . 2013,第5期

机译：在最初受到高度干扰的亚音速射流中，确定喷嘴出口边界层厚度及其相应的雷诺数的影响
3. Effects of moderate Reynolds numbers on subsonic round jets with highly disturbed nozzle-exit boundary layers [J] . Bogey C., Marsden O., Bailly C. Physics of fluids . 2012,第10期

机译：中等雷诺数对具有高度扰动的喷嘴出口边界层的亚音速圆形射流的影响
4. Influence of nozzle-exit boundary-layer profile on high-subsonic jets [C] . Christophe Bogey, Olivier Marsden AIAA/CEAS aeroacoustics conference;AIAA aviation forum . 2014

机译：喷嘴出口边界层轮廓对高亚音速射流的影响
5. Thermally induced instability to enhance boundary layer turbulence intensity using heat sources and spires to create boundary layer turbulence intensity and control [D] . Yarlagadda, Goutham Kumar. 2016

机译：热诱导不稳定性以增强热源和尖端的边界层湍流强度，以产生边界层湍流强度和控制
6. New Electrospinning Nozzle to Reduce Jet Instability and Its Application to Manufacture of Multi-layered Nanofibers [O] . Byoung-Sun Lee, Seung-Yeol Jeon, Haedong Park, -1

机译：减少射流不稳定性的新型静电纺丝喷嘴及其在多层纳米纤维制造中的应用
7. Effects of nozzle-exit boundary-layer profile on the initial shear-layer instability, flow field and noise of subsonic jets [O] . Christophe Bogey, Roberto Sabatini 2019

机译：喷嘴 - 出口边界层轮廓对初剪缺陷，流场和亚音速喷射噪声的影响

Investigation of the effect of turbulence intensity and nozzle exit boundary layer thickness on stability pattern of subsonic jet

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