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Shear layer control in a free-vortex aerodynamic window

机译:自由涡流气动窗口中的剪切层控制

摘要

A boundary-controlled aerodynamic window positioned adjacent the exit aperture of a gas laser is transparent to the laser beam emitted from the cavity of the laser. The boundary-controlled aerodynamic window is formed by a high velocity gas flow directed by a duct across the exit aperture for the laser beam isolating the low pressure region of the cavity from the high pressure of the atmosphere. The exit aperture is enlarged and an auxiliary gas flow injected along the sidewall of the duct adjacent the exit aperture to expand the thickness of the boundary layer. In a second embodiment, particulate matter is fixedly attached to the sidewall of the duct to increase the roughness of the wall surface. A third embodiment uses a plurality of nozzles, each injecting gas with a predetermined velocity.
机译:位于气体激光器出口附近的边界控制空气动力学窗口对从激光器腔发出的激光束透明。边界控制的空气动力学窗口是由高速气流形成的,该高速气流由穿过出口孔的导管引导,用于激光束将空腔的低压区域与大气的高压隔离开。出口孔扩大,并且沿着邻近出口孔的管道的侧壁注入辅助气流以扩大边界层的厚度。在第二实施例中,颗粒物质被固定地附接到管道的侧壁以增加壁表面的粗糙度。第三实施例使用多个喷嘴,每个喷嘴以预定速度喷射气体。

著录项

  • 公开/公告号US4559628A

    专利类型

  • 公开/公告日1985-12-17

    原文格式PDF

  • 申请/专利权人 UNITED TECHNOLOGIES CORPORATION;

    申请/专利号US19830488838

  • 发明设计人 BRUCE V. JOHNSON;ROY N. GUILE;

    申请日1983-04-26

  • 分类号H01S3/08;

  • 国家 US

  • 入库时间 2022-08-22 07:29:44

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