Hostname: page-component-cd9895bd7-gxg78 Total loading time: 0 Render date: 2024-12-28T05:42:38.864Z Has data issue: false hasContentIssue false
  • English
  • Français

Helicopter Stability in Hovering Flight

Published online by Cambridge University Press:  28 July 2016

A. R. S. Bramwell
Get access Rights & Permissions [Opens in a new window]

Extract

In view of the strong claims for offset flapping and drag hinges made by Mr. Payne in his Technical Note (September 1955) I would like to make the following comments.

Many of his conclusions depend on the assertion that there is a steady inertia force on the rotor hub when the rotor tilts. This force is simply the reaction on the hub due to the sideways thrust component and should not be included with the external forces on the helicopter.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 60 , Issue 548 , August 1956 , pp. 549 - 550
Copyright
Copyright © Royal Aeronautical Society 1956

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)