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The effect of roughness of blunted nose of cone on the development of disturbances and laminar-turbulent transition in a hypersonic boundary layer

机译：锥体粗糙度粗糙度对超声边界层中扰动和层流湍流过渡的影响

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Yu. Gromyko; D. Bountin; P. Polivanov; A. Sidorenko; A. Maslov;
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1. Influence of blunt-cone tip temperature on the laminar-turbulent transition in hypersonic boundary layers [J] . D.A. Bountin, Yu.V. Gromyko, S.V. Kirilovskiy, Thermophysics and Aeromechanics . 2018,第4期

机译：钝锥尖端温度对高音界边界层层流湍流过渡的影响
2. Stability analysis and transition prediction of hypersonic boundary layer over a blunt cone with small nose bluntness at zero angle of attack [J] . SU Cai-hong, ZHOU Heng 应用数学和力学（英文版） . 2007,第005期

机译：零迎角小鼻钝的钝锥上高超声速边界层的稳定性分析和过渡预测
3. Effect of the Cone Nose Bluntness and the Ultrasonically Absorptive Coating on Transition in a Hypersonic Boundary Layer [J] . D. A. Buntin, S. V. Lukashevich, A. A. Maslov, Fluid Dynamics . 2010,第6期

机译：锥鼻钝度和超声吸收涂层对高超声速边界层过渡的影响
4. The effect of roughness of blunted nose of cone on the development of disturbances and laminar-turbulent transition in a hypersonic boundary layer [C] . Yu. Gromyko, D. Bountin, P. Polivanov, Conference on High-Energy Processes in Condensed Matter . 2017

机译：锥体粗糙度粗糙度对超声边界层中扰动和层流湍流过渡的影响
5. Numerical investigation of laminar-turbulent transition in a cone boundary layer at mach 6 [D] . Sivasubramanian, Jayahar 2012

机译：6马赫圆锥边界层内层流湍流的数值研究
6. Effect of a Roughness Element on the Receptivity of a Hypersonic Boundary Layer over a Blunt Cone Due to Pulse Entropy Disturbance with a Single Frequency [O] . Zhenqing Wang, Mingfang Shi, Xiaojun Tang, 2018

机译：粗糙元件对钝锥体上超声边界层的接受性的影响由于单频脉冲熵干扰
7. Effect of a Roughness Element on the Receptivity of a Hypersonic Boundary Layer over a Blunt Cone Due to Pulse Entropy Disturbance with a Single Frequency [O] . Zhenqing Wang, Mingfang Shi, Xiaojun Tang, 2018

机译：粗糙元件对钝锥体上超声边界层的接受性的影响，由于单频脉冲熵干扰
8. Artificially Induced Boundary-Layer Transition on Blunt-Slender Cones Using Distributed Roughness and Spherical-Type Tripping Devices at Hypersonic Speeds. [R] . boudreau, a. h. 1978

机译：利用分布式粗糙度和球形跳闸装置在超音速速度下人工诱导钝角锥体上的边界层过渡。

The effect of roughness of blunted nose of cone on the development of disturbances and laminar-turbulent transition in a hypersonic boundary layer

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