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METHOD FOR FINDING WING TYPE BY USING WIND TUNNEL AND WING TYPE MODEL FOR WIND TUNNEL TEST

机译:风洞试验的翼型识别方法及风洞试验的翼型模型

摘要

PURPOSE:To find a wing type which provides a target pressure distribution and to improve design accuracy and to shorten a design period by correcting the flexible surface of the wing type during air blasting in a wind channel. CONSTITUTION:During the air blasting in the wind tunnel, pressure is measured through plural static pressure holes 4 and inputted to an electronic computer 6, which calculates the difference from the target pressure distribution and computes shape correction quantities by reverse solution calculation, so that a shape correction signal is obtained from the electronic computer 6. Respective actuators 2 are put in operation with the signal and the flexible surface 3 of the model 1 is deformed to correct the wing type of the model 1 so that the target pressure distribution is realized.
机译:目的:寻找一种能够提供目标压力分布的机翼类型,并通过在风道中进行鼓风期间校正机翼类型的柔性表面来提高设计精度并缩短设计周期。组成:在风洞中进行鼓风期间,通过多个静压孔4测量压力,并将其输入到电子计算机6中,该计算机计算与目标压力分布的差值,并通过反向求解计算来计算形状校正量,因此形状校正信号是从电子计算机6获得的。相应的致动器2都在该信号下运行,模型1的柔性表面3变形以校正模型1的机翼类型,从而实现目标压力分布。

著录项

  • 公开/公告号JPH039236A

    专利类型

  • 公开/公告日1991-01-17

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY IND LTD;

    申请/专利号JP19890142203

  • 发明设计人 TATSUMI SHIGEFUMI;

    申请日1989-06-06

  • 分类号G01M9/08;

  • 国家 JP

  • 入库时间 2022-08-22 05:59:53

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