Hostname: page-component-78c5997874-94fs2 Total loading time: 0 Render date: 2024-11-09T09:10:32.822Z Has data issue: false hasContentIssue false

Limitations in Helicopter Design

Published online by Cambridge University Press:  26 October 2023

Extract

Core share and HTML view are not available for this content. However, as you have access to this content, a full PDF is available via the ‘Save PDF’ action button.

Ladies and Gentlemen,

As most of you know this is the Fourth and last lecture of our present session, the other three having been given by Gp/Capt. LIPTROT, Mr. C. G. PULLIN and Mr. R. A. C. BRIE, covering an historical survey, design and operation of helicopters, etc., and to-day our lecturer is discussing “Limitations in Helicopter Design.”

It gives me very great pleasure to introduce Dr. BENNETT to you, for I have known him personally for fifteen years or more, during the whole of which time he has been intimately associated with rotary wing and helicopter design.

For some years prior to the war, Dr. BENNETT was with Messrs. G. & J. Weir and the Cierva Autogiro Co.; and during the war was C.T.O. at the Airborne Forces Experimental Establishment and spent two years in the U.S.A. where he latterly was attached to Wright Field as project engineer on helicopter research.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1947