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Wind tunnel performance comparative test results of a circular cylinder and 50 ellipse tailboom for circulation control antitorque applications

机译:圆柱和50%椭圆尾杆用于循环控制反扭矩应用的风洞性能对比测试结果

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摘要

A low speed wind tunnel study to quantitatively evaluate the performance (lift and drag) of a circular cylinder and comparable 50% ellipse was conducted. Circular cylinder performance was evaluated at slot positions of 80 deg to 135 deg, measured relative to freestream; 50% ellipse performance was measured for angles of attack between -5 deg and 30 deg. Tests were conducted at three blowing coefficients, 0.3, 0.4 (optimal historically) and 0.5, to evaluate tailboom performance sensitivity. Circulation control test results revealed optimal c1 values at an approximate 116 deg slot position, corresponding to cd values no greater than that of a smooth cylinder. The 50% ellipse results revealed optimal c1 values at approximately 18 deg AOA, though associated with considerable drag. For all three blowing coefficients, the circular cylinder L/D values were consistently three to four times greater than their 50% ellipse counterparts. Recommendations for future NOTAR(TM) tailboom design modifications and later research are made.
机译:进行了低速风洞研究,以定量评估圆柱体的性能(升力和阻力),并得出可比较的50%椭圆形。在相对于自由流测量的80度至135度的槽位置处评估了圆柱体的性能;对于-5度和30度之间的迎角,测量了50%的椭圆性能。在三个吹气系数(0.3、0.4(历史上最佳)和0.5)下进行了测试,以评估尾杆性能灵敏度。循环控制测试结果表明,最佳的c1值位于大约116度的槽位置,对应的cd值不大于平滑圆柱的cd值。 50%的椭圆结果显示最佳的c1值在大约18度AOA处,尽管与相当大的阻力相关。对于所有三个吹气系数,圆柱体的L / D值始终比其50%椭圆对应值大三到四倍。提出了有关将来的NOTAR(TM)尾杆设计修改和以后的研究的建议。

著录项

  • 作者

    Fisher David T.;

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  • 年度 1994
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  • 原文格式 PDF
  • 正文语种 en_US
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