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Method of wind tunnel measurement of airfoil

机译:翼型的风洞测量方法

摘要

A method of wind tunnel measurement of airfoil, includes a step of providing a wind tunnel test apparatus. The wind tunnel test apparatus includes two walls, two supporting members, and two load measuring units. The method further includes steps of: coupling both ends of an airfoil model under test with the two supporting members, respectively; generating a flow of a fluid in the wind tunnel flow path; and measuring a load applied to the airfoil model by using the two load measuring units. A thin film member is stuck on each end of the airfoil model so that a part of the thin film member protrudes from the each end of the airfoil model along an outer circumference throughout an entire circumference. The thin film member has a strength at which the thin film member enables to endure a pressure of the fluid, and is formed of a material which is elastically deformable. The thin film member is provided so that a gap between the each end of the airfoil model and one of the two walls facing to the each end of the airfoil model is blocked.
机译:一种翼型的风洞测量方法,包括提供风洞测试设备的步骤。风洞测试设备包括两个壁,两个支撑构件和两个载荷测量单元。该方法还包括以下步骤:将被测机翼模型的两端分别与两个支撑构件连接;在风洞流路中产生流体流;通过使用两个载荷测量单元,测量施加到翼型模型上的载荷。薄膜构件粘贴在翼型模型的每个端部上,使得一部分薄膜构件从翼型模型的每个端部沿着整个整个圆周沿外周突出。薄膜构件具有使薄膜构件能够承受流体的压力的强度,并且由可弹性变形的材料形成。设置薄膜构件以使得翼型模型的每个端部与面对翼型模型的每个端部的两个壁之一之间的间隙被阻塞。

著录项

  • 公开/公告号US8359916B2

    专利类型

  • 公开/公告日2013-01-29

    原文格式PDF

  • 申请/专利权人 KAI KARIKOMI;YOSUKE NAKAMURA;

    申请/专利号US20100963978

  • 发明设计人 YOSUKE NAKAMURA;KAI KARIKOMI;

    申请日2010-12-09

  • 分类号G01M9/00;

  • 国家 US

  • 入库时间 2022-08-21 16:43:48

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