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An Experimental Investigation of Nozzle-Exit Boundary Layers of Highly Heated Free Jets

机译：高加热自由射流喷嘴出口边界层的实验研究

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J. Lepicovsky;
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年度 2016
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1. 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
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. Experimental investigation of the free convection velocity boundary layer and plume formation region for a heated horizontal cylinder [J] . Joel P. Kuehner, A.M. Hamed, Jared D. Mitchell International Journal of Heat and Mass Transfer . 2015,第mara期

机译：水平加热圆柱体自由对流速度边界层和羽流形成区域的实验研究
4. Effects of Disturbed Nozzle-exit Boundary Layers on Acoustic Waves from Ideally-expanded Supersonic Jet [C] . Taku Nonomura, Akira Oyama, Kozo Fujii, AIAA/CEAS aeroacoustics conference . 2016

机译：理想扩展的超音速射流对扰动的喷嘴出口边界层对声波的影响
5. THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE ISOTHERMAL AXISYMMETRIC TURBULENT FREE JET (CIRCULAR, BOUNDARY). [D] . BELL, DAVID A. 1984

机译：等温轴对称湍流自由射流（圆形，边界）的理论和实验研究。
6. Experimental Investigation on Velocity and Temperature Field in a Rotating Non-isothermal Turbulent Boundary Layer using Hot-wire [O] . Li Gangfu, Li Haiwang, You Ruquan, -1

机译：旋转非等温湍流边界层热线速度和温度场的实验研究
7. Effects of moderate Reynolds numbers on subsonic round jets with highly disturbed nozzle-exit boundary layers [O] . Christophe Bogey, Olivier Marsden, Christophe Bailly 2012

机译：高度雷诺数对高度扰动喷嘴出口边界层亚圆形喷射的影响

An Experimental Investigation of Nozzle-Exit Boundary Layers of Highly Heated Free Jets

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