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首页> 外文期刊>Journal of Aircraft >Lifting-Line Predictions for Induced Drag and Lift in Ground Effect
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Lifting-Line Predictions for Induced Drag and Lift in Ground Effect

机译:地面效应引起的阻力和举升的举升线预测

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摘要

Closed-form relations are presented for estimating ratios of the induced-drag and lift coefficients acting on a wing in ground effect to those acting on the same wing outside the influence of ground effect The closed-form relations for these ground-effect influence ratios were developed by correlating results obtained from numerical solutions to Prandtl's lifting-line theory. Results show that these influence ratios are not unique functions of the ratio of wing height to wingspan, as is sometimes suggested in the literature. These ground-effect influence ratios also depend on the wing planform, aspect ratio, and lift coefficient
机译:提出了闭合形​​式关系,以估计作用于机翼在地面效应中的感应阻力系数和升力系数与作用在同一翼上的引力系数和外部系数在地面效应影响之外的比率。通过将数值解获得的结果与Prandtl的提升线理论相关联来开发。结果表明,这些影响比并不是机翼高度与翼展之比的唯一函数,正如文献中有时所暗示的那样。这些地面效应影响比还取决于机翼平面形状,纵横比和升力系数

著录项

  • 来源
    《Journal of Aircraft》 |2013年第4期|1226-1233|共8页
  • 作者

    W. F. Phillips; D. F. Hunsaker;

  • 作者单位

    Mechanical and Aerospace Engineering Department, 4130 Old Main Hill,Utah State University, Logan, Utah 84322-4130;

    1624 Flight Line,Scaled Composites, Mojave, California 93501-1663;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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