Hostname: page-component-78c5997874-fbnjt Total loading time: 0 Render date: 2024-11-06T07:10:19.005Z Has data issue: false hasContentIssue false
  • English
  • Français

Rotorcraft Work at the Aeroplane and Armament Experimental Establishment

Published online by Cambridge University Press:  04 July 2016

J. Poole
J. Poole*
Affiliation:
Performance Division, Aeroplane and Armament Experimental Establishment
Get access Rights & Permissions [Opens in a new window]

Extract

The A. & A.E.E. has been associated with rotorcraft in this country almost from their earliest days. For example, the records show that a C30A Autogiro was evaluated at Martlesham Heath in 1935. After the outbreak of war responsibility for development work in the rotary wing field was assumed by the Airborne Forces Establishment (later the Airborne Forces Experimental Establishment) and the accounts of such developments as the Rotachute and the airborne jeep have since become well known. In 1945 the A.F.E.E. was declared to be the official testing establishment for prototype helicopters and this responsibility has remained until the present time. The A.F.E.E. was merged in 1951 with the A. & A.E.E., becoming the Airborne and Helicopter Division of the latter Establishment.

Type
Rotorcraft Section
Information
The Aeronautical Journal , Volume 67 , Issue 632 , August 1963 , pp. 501 - 513
Copyright
Copyright © Royal Aeronautical Society 1963

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.)

References

1.Brie, R.Some Problems of Helicopter Operation and Their Influence on Design. Journal of the Helicopter Association of Great Britain. 1947.Google Scholar
2.Fitzwilliams, O. L. L.Some Work with Rotating Wing Aircraft. Journal of the Helicopter Association of Great Britain. 1947.Google Scholar
3.O'Hara, F.Flight Testing of Helicopters. Journal of the Helicopter Association of Great Britain. 1950.Google Scholar
4.Gellatly, W. R.Some Handling Aspects Introduced by Increased Helicopter Requirements. Journal of the Helicopter Association of Great Britain. 1953.CrossRefGoogle Scholar
5.O'Hara, F.Helicopter Research. Journal of the Helicopter Association of Great Britain. 1954.Google Scholar
6.Webb, H. J.Some Engineering Aspects of Helicopter Assessment Trials. Journal of the Helicopter Association of Great Britain. 1959.CrossRefGoogle Scholar
7.Kinchella, F. C. A Comprehensive Method of Helicopter Performance Reduction. Unpublished A. & A.E.E. Note, July 1958.Google Scholar
8.O'hara, F. A Method of Performance Reduction for Helicopters. R. & M. 2770, October 1947.Google Scholar
9.Wilkinson, D. A. Some Aspects of Night and Instrument Flying on Single Rotor Helicopters. Unpublished A. & A.E.E Report.Google Scholar
10.Scanlon, J.Flight Requirements for the Operation of Rotorcraft. Journal of the Royal Aeronautical Society, April 1963.Google Scholar
11.Gregory, J. D. L. and Coombes, R. W. An Account of Some Longitudinal Stability Tests on a Dragonfly Helicopter. Unpublished A. & A.E.E. Report.Google Scholar