...
【24h】

Aerodynamic Forum

机译:空气动力学论坛

获取原文
获取原文并翻译 | 示例

摘要

Last month I went on at length about flaps and airbrakes, and managed to cover just the bare essentials, in answer to a question from Syd Yates. I promised to do the same for leading edge devices, some of which are illustrated in Figure 1. The simplest device 'A' is a small aerofoil section, or even a thin curved plate, fixed ahead of the leading edge to form a converging slot. Instead of adding to the wing, a slot may be cut through the section itself as in 'B' to form the slot. Fixed devices cause unnecessary drag at high speed so the retractable slat was invented. When retracted it forms part of the optimised aerofoil and is intended to be deployed to form the slot only at low speed. A clever variation of this, allegedly invented by Handley Page, is the automatic slat designed to pop open at low speed when the stagnation point moves down to its opening. They also tended to pop open when pulling g so could be locked for aerobatics.
机译:上个月,我回答了赛德·耶茨(Syd Yates)的一个问题,继续详细介绍了襟翼和气闸,并设法只涵盖了基本要素。我答应对前沿设备执行相同的操作,其中一些如图1所示。最简单的设备“ A”是翼型较小的截面,甚至是薄的弯曲板,都固定在前沿之前以形成会聚槽。除了在机翼上添加外,还可以像在“ B”中那样在截面本身上切一个槽以形成槽。固定设备会导致不必要的高速拖动,因此发明了可伸缩板条。当缩回时,它形成了优化的机翼的一部分,旨在仅在低速时展开以形成狭缝。据称由亨德利·佩奇(Handley Page)发明的一种巧妙的变化是,当停滞点下降到其开口处时,自动板条设计为以低速弹出。它们在拉动g时也倾向于弹出,因此可能会被锁定以进行特技飞行。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号