Hostname: page-component-68945f75b7-gkscv Total loading time: 0 Render date: 2024-08-06T02:13:58.413Z Has data issue: false hasContentIssue false
  • English
  • Français

Problems Associated with the Strength Assessment of Rotor Blades

Published online by Cambridge University Press:  26 October 2023

V A B Rogers
V A B Rogers*
Affiliation:
The Fairey Aviation Company Ltd
Get access

Extract

The Chairman, in introducing the Author, described the subject of his paper as one of paramount importance to all who were concerned in the design and operation of helicopters Mr Rogers was an indentured aeronautical engineer apprentice at the Fairey Aviation Company from 1940 to 1946, during which time he obtained the Ordinary and Higher National Certificates in Mechanical and Aeronautical Engineering He was awarded an S B A C scholarship to the College of Aeronautics in 1946 and obtained a diploma with distinction in Aircraft Design

Type
Research Article
Information
The Journal of the Helicopter Association of Great Britain , Volume 11 , Issue 4 , August 1957 , pp. 189 - 222
Copyright
Copyright © Royal Aeronautical Society 1957

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.)

Footnotes

*

A rectangular flight envelope is now defined for rotary wing aircraft in A P 970 Vol 3