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Improvements in or relating to fluid-solid contact-surfaces

机译:改进或涉及流固接触表面

摘要

578,763. Reducing surface friction between a solid and a fluid. GRIFFITH, A. A. Aug. 25, 1942, No. 11973. [Class 4] To improve the effect of slots provided for the removal by suction of the boundary layer of fluid from surfaces such as those of aeroplanes, pumps, compressors and turbines, that are movable relatively to the fluid, the surface is so shaped that no rise of pressure occurs on the surface in the general direction of flow except in the region between a slot and its associated stagnation point where the flow of the boundary layer is locally reversed in direction. This may be done by providing that the surface curvature suddenly changes in passing across the slot so that it is less convex on the downstream side of the slot. In the example shown, the parts 23, 24 of the surface on the upstream and downstream side of a slot 13 are convex and concave respectively and the slot is tangential to the curve 24. There is thus no rise of pressure except as shown by the pressure curve P at 19, between the slot and the stagnation point 18 and the pressure falls gradually as indicated at 25, from the stagnation point to the next slot downstream. A fan 26 is provided for producing suction in the slots. With a surface and slots so formed and arranged, there is no fall and subsequent rise of pressure between the stagnation point and the next slot such as is shown to exist with the usual slotted surface. In a modification, the slots are wider than is necessary for the removal of the boundary layer and there is a sharp edge between the convex surface 23 and the upper flat wall of the slot.
机译:578,763。减少固体和流体之间的表面摩擦。 GRIFFITH,AA,1942年8月25日,第11973号。[第4类]为了改善通过抽吸飞机,泵,压缩机和涡轮机等表面上的流体边界层而去除缝隙的效果,相对于流体是可移动的,该表面的形状使得除了在狭缝及其相关的停滞点之间的区域(边界层的流动在此处局部反向)之外,在整个流动方向上在表面上不会出现压力升高。方向。这可以通过以下方式来实现:提供表面曲率在穿过狭槽时突然改变,从而在狭槽的下游侧凸度较小。在所示的示例中,狭槽13的上游侧和下游侧的表面的部分23、24分别是凸的和凹的,并且该狭槽与曲线24相切。因此,除了由在槽和停滞点18之间的19处的压力曲线P,压力从停滞点到下游的下一个槽逐渐减小,如25所示。提供风扇26以在狭槽中产生吸力。具有如此形成和布置的表面和狭缝,在停滞点和下一个狭缝之间不会出现压力的下降和随后的升高,例如显示为具有通常的狭缝表面。在一个变型中,狭槽比去除边界层所需的狭槽宽,并且在凸面23和狭槽的上平坦壁之间存在尖锐的边缘。

著录项

  • 公开/公告号GB578763A

    专利类型

  • 公开/公告日1946-07-11

    原文格式PDF

  • 申请/专利权人 ALAN ARNOLD GRIFFITH;

    申请/专利号GB19420011973

  • 发明设计人

    申请日1942-08-25

  • 分类号B64C21/06;

  • 国家 GB

  • 入库时间 2022-08-24 03:03:24

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