Hostname: page-component-cd9895bd7-gvvz8 Total loading time: 0 Render date: 2024-12-22T15:57:03.459Z Has data issue: false hasContentIssue false

The Work of the Royal Aircraft Establishment

Published online by Cambridge University Press:  04 July 2016

L. F. Nicholson*
Affiliation:
Royal Aircraft Establishment Royal Aircraft

Extract

To write a paper on the work of the Royal Aircraft Establishment is a formidable task. To summarise the programme of work of the Establishment would either provide material for a series of lectures or, if compressed to a single lecture, would lead to a cursory and superficial treatment. I make no apologies, therefore, for not attempting any sort of complete survey. Within the scope of this lecture all I intend to do is to give a brief description of the RAE, what it is, what it does and how it is organised and then to consider a few items drawn from three of the RAE's research programmes, which have been selected to show some of the characteristics of the RAE and the kind of work which goes on there.

The first series of items to be presented fall in the field of the slender wing. The great potentiality of the slender wing for a wide range of applications was apparent from the time the concept was first considered. What I want to stress is the enormous range of detailed researches which are required before such a concept can be used in practical designs.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1965

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.Küchemann, D.Aircraft Shapes and Their Aerodynamics for Flight at Supersonic Speeds. Proceedings of the 2nd International Congress of Aeronautical Sciences Zurich, 1960. Pergamon Press.Google Scholar
2.Maskell, E. C. and Weber, J.On the Aerodynamic Design of Slender Wings. Journal of the Royal Aeronautical Society, Vol. 63, p 709, December 1959.CrossRefGoogle Scholar
3.Spence, A. and Lean, D.Some Low Speed Problems of High Speed Aircraft. Journal of the Royal Aeronautical Society, Vol. 66, p 211, April 1962.CrossRefGoogle Scholar
4.Earnshaw, P. B. An Experimental Investigation of the Structure of a Leading Edge Vortex. R & M No. 3281, 1962.Google Scholar
5.Waters, M. H. L. and Holford, J. F. Some Technical Factors Influencing the Direct Operating Costs of a Medium Range Civil Jet Transport. Proceedings of the Symposium on Short Range Transport Aircraft. Indian Aeronautical Society, December 1964to be published.Google Scholar
6.Nicholson, L. F. Some Considerations of Economical Short Range Transport Aircraft. Proceedings of the Symposium on Short Range Transport Aircraft. Indian Aero nautical Society, December 1964to be published.Google Scholar