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Design of Vortex Generator Flow Control in Inlets

机译:进风口涡流发生器流量控制设计

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摘要

This article summarizes the results of an optimization study of a microvortex generator flow control in an inlet. Five parameters optimization was carried out using the classical design of experiment method. Two main objectives were in focus: first, to develop the methodology and skills necessary to conduct a design of experiment optimization study in area of the flow control; and second, to develop the procedures which would be used during design of vortex generator flow control in inlets. New information about the dependency of the vortex generator flow control in inlet on its geometrical parameters were obtained. Several interesting configurations were located. The parameters of optimal settings were then used to set up the vortex generator installation in a generic inlet.
机译:本文总结了进气口微涡流发生器流量控制的优化研究结果。使用经典的实验方法设计进行了五个参数优化。重点关注两个主要目标:第一,开发进行流量控制领域的实验优化研究设计所需的方法和技能;第二,开发在进气道涡流发生器流量控制设计中将使用的程序。获得了有关入口处涡流发生器流量控制对其几何参数的依赖性的新信息。找到了几个有趣的配置。然后,将最佳设置参数用于在通用进气口中设置涡流发生器安装。

著录项

  • 来源
    《Journal of Aircraft》 |2006年第6期|p.1886-1892|共7页
  • 作者

    Adam Jirasek;

  • 作者单位

    Swedish Defence Research Agency FOI, 164 90 Stockholm, Sweden;

  • 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 航空;
  • 关键词

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