高超声速风洞试验模型底压测量方法研究

谢飞, 郭雷涛, 张绍武, 曹程, 邹琼芬

谢飞, 郭雷涛, 张绍武, 曹程, 邹琼芬. 高超声速风洞试验模型底压测量方法研究[J]. 实验流体力学, 2016, 30(4): 71-75. DOI: 10.11729/syltlx20150043
引用本文: 谢飞, 郭雷涛, 张绍武, 曹程, 邹琼芬. 高超声速风洞试验模型底压测量方法研究[J]. 实验流体力学, 2016, 30(4): 71-75. DOI: 10.11729/syltlx20150043
Xie Fei, Guo Leitao, Zhang Shaowu, Cao Cheng, Zou Qiongfen. Study on model base pressure measuring technique in hypersonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(4): 71-75. DOI: 10.11729/syltlx20150043
Citation: Xie Fei, Guo Leitao, Zhang Shaowu, Cao Cheng, Zou Qiongfen. Study on model base pressure measuring technique in hypersonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(4): 71-75. DOI: 10.11729/syltlx20150043

高超声速风洞试验模型底压测量方法研究

详细信息
    通讯作者:

    谢飞(1980-),男,重庆长寿人,工程师。研究方向:高超声速风洞气动力试验技术研究。通信地址:四川省绵阳市中国空气动力研究与发展中心(621000)。E-mail:feixiefei@sohu.com

  • 中图分类号: V211.752

Study on model base pressure measuring technique in hypersonic wind tunnel

  • 摘要: 针对高超声速风洞试验模型底压测量误差较大而导致模型底阻难以精确扣除的问题,在Φ1m高超声速风洞中开展了3种底压测量方法的对比研究,即电子扫描压力测量方法、低压力差压传感器测量方法和微型绝压传感器测量方法,并在马赫数6试验条件下开展了HB-2标模和某导弹模型试验验证。试验结果表明:采用微型绝压传感器进行模型底部压力测量能避免测压管路的影响,可快速响应高超声速风洞试验模型底部压力变化情况,有效提高模型底压的测量精准度。
    Abstract: It is an experimental technique problem to exactly achieve test model base pressure in hypersonic wind tunnel. Because of the large error of model base pressure measurement before, it is difficult to exactly deduct the model base drag. Three base pressure measuring methods are developed in Φ1m hypersonic wind tunnel, viz. the absolute pressure micro-sensor measuring method, the low pressure differential pressure sensor measuring method and the electronic scanning pressure (ESP) measuring method. The validation tests of HB-2 standard model and a certain missile model are separately conducted at Ma=6. The test results indicate that: the absolute pressure micro-sensor measuring method can avoid the influence of piezometric pipe; it also can rapidly respond the variation of model base pressure with high accuracy.
  • 图  1   电子扫描压力测量系统硬件组成框图

    Fig.  1   Electronic scanning pressure system

    图  2   CYG220T差压传感器

    Fig.  2   CYG220T differential pressure sensor

    图  3   CYG504A微型绝压传感器

    Fig.  3   CYG504A absolute micro-pressure sensor

    图  4   HB-2标模底压测量装置实物照片

    Fig.  4   HB-2 standard model base pressure measuring device

    图  5   HB-2标模3种方法底压测量结果对比曲线

    Fig.  5   Comparison of HB-2 standard model base pressure measuring results

    图  6   某导弹模型2种方法底压测量结果对比曲线

    Fig.  6   Comparison of X missile model base pressure measuring results

    图  7   HB-2标模pb~α曲线

    Fig.  7   Base pressure variations with attcak angle of HB-2 standard model

    图  8   某导弹模型pb~α曲线

    Fig.  8   Base pressure variations with attcak angle of X missile model

    表  1   HB-2标模3种底压方法测量重复性对比

    Table  1   Measuring results of HB-2 base pressure

    项目α/(°)电子扫描阀差压传感器绝压传感器
    平均值/Pa-4195212224
    0213238247
    4180198227
    8112134164
    126182120
    标准差/Pa-41177
    01066
    41086
    8896
    12968
    重复性偏差/%-410.35.95.7
    09.454.9
    49.46.74.9
    87.57.64.9
    128.556.5
    下载: 导出CSV

    表  2   某导弹模型2种底压方法测量重复性对比

    Table  2   Measuring results of X missile model base pressure

    项目α/(°)电子扫描阀绝压传感器
    pb1pb2pb1pb2
    平均值/Pa-14563534501458
    -10525498418375
    -6552524427405
    -4595566449436
    -2630598466456
    0674643493485
    2683653474467
    4704671474468
    标准差/Pa-14272478
    -10242685
    -6242436
    -4283157
    -2293153
    0353763
    2394130
    442445
    重复性偏差/%-147.76.92.83.1
    -106.87.33.42.2
    -66.96.81.12.5
    -47.98.92.22.8
    -28.28.92.21.1
    01010.52.51.4
    211.211.61.20.1
    41212.51.90.9
    下载: 导出CSV
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出版历程
  • 收稿日期:  2015-03-22
  • 修回日期:  2015-11-21
  • 刊出日期:  2016-08-24

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