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- Consequently, secondary instability is unlikely the main cause leading to transition in supersonic boundary layers. 因此,二次失稳应该不是导致超音速边界层转捩的主要因素。
- Parabolized stability equations (PSE) approach is used to investigate problems of secondary instability in supersonic boundary layers. 摘要用抛物化稳定性方程(PSE)研究超音速边界层中的二次失稳问题。
- A study of the boundary condition in the DNS of the supersonic boundary layer flow 超声速边界层流动数值模拟的边界条件研究
- Study of the Mechanism of Breakdown in Laminar-Turbulent Transition of a Supersonic Boundary Layer on a Flat Plate 超音速平板边界层转捩中层流突变为湍流的机理研究
- Numerical Study for the Resonant Triad Interaction and Secondary Instability in a Two-Dimensional Supersonic Boundary Layer 二维超音速边界层中三波共振和二次失稳机制的数值模拟研究
- supersonic boundary layer 超音速边界层
- Sound Propagation in the Nocturnal Boundary Layer. 夜间边界层中的声传播。
- Detection of Boundary Layer Water Clouds by Spaceborne Cloud Radar. 用机载云雷达探测边界层含水云。
- Beyond the boundary layer, the motion is highly irregular. 超出边界层以外,流体的流动非常没有规律。
- Formulation of Turbulent Fluxes in the Stable Boundary Layer. 稳定边界层中湍流通量算法。
- Stull, R.B., 1988: An introduction to boundary layer meteorology. 任平,2003:影响大气污染物散布的气象条件。
- As the air proceeds along the test section the boundary layer thickens. 当空气沿着试验段流动时附面层逐渐变厚。
- supersonic sharp cone boundary layer 超音速尖锥边界层
- supersonic boundary surface transmitter 超声界面变送器
- The Contribution of Shear to the Evolution of a Convective Boundary Layer. 切变对对流边界层演变的作用。
- A systematic study of TiO2 ceramic boundary layer capacitor (BLC) ismade. 本文对TiO_2陶瓷晶界层电容器进行了较为系统的研究。
- To solve this problem, a boundary layer suction test is carried out. 为此,本文采用附面层抽吸技术对其进行了地面抽吸状态下的流场控制试验研究。
- The bell reducer provides the cyclone action and the boundary layer control. 喇叭形异径管产生旋风作用并进行边界层控制。
- The evolution of vortexes in the boundary layer are numerically simulated. 本文数值模拟了多涡结构在边界层中的非线性演化过程。
- A separation in the boundary layer of fluid about a moving streamlined body, such as the wing of an airplane, causing a breakdown in the smooth flow of fluid and resulting in turbulence. 气流分离移动的流线型的躯体上流体边界层上的分隔物,如飞机的机翼,在平滑的流体流动中会引起故障和湍流