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首页> 外文期刊>Journal of Aircraft >Stability of Lobed Superpressure Balloons During Ascent
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Stability of Lobed Superpressure Balloons During Ascent

机译:上升过程中打滑的超压气球的稳定性

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摘要

It is known from large-scale experiments that the successful deployment of lobed superpressure balloons can depend on the used gas. Some balloons deployed properly during an inflation with air but failed to reach the desired equilibrium configuration for helium. Furthermore, depending on the desired flight altitude, a helium-filled balloon might or might not deploy properly. This paper investigates this phenomenon by studying the stability of lobed superpressure balloons during ascent. It is shown that wrinkles increasingly reduce the stiffness of balloons for a decreasing gas density and an increasing flight altitude such that clefts can develop at very low differential pressures in nearly fully inflated balloons.
机译:从大规模实验中可以知道,成叶的超压气球的成功部署取决于所用的气体。一些气球在充入空气期间正确部署,但未能达到所需的氦气平衡构型。此外,根据所需的飞行高度,充氦的气球可能会也可能不会正确部署。本文通过研究有瓣超压气球在上升过程中的稳定性来研究这种现象。结果表明,随着气体密度的降低和飞行高度的增加,皱纹逐渐降低了气球的刚度,从而在几乎完全充气的气球中,在非常低的压差下会产生裂痕。

著录项

  • 来源
    《Journal of Aircraft》 |2011年第6期|p.2042-2049|共8页
  • 作者

    Markus Pagitz;

  • 作者单位

    Delft University of Technology, 2629 HS Delft, The Netherlands;

  • 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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