Hostname: page-component-848d4c4894-mwx4w Total loading time: 0 Render date: 2024-06-30T16:59:33.181Z Has data issue: false hasContentIssue false

A new shape in the sky

Published online by Cambridge University Press:  04 July 2016

Extract

May I thank the Society for the immense compliment it has paid me tonight by the award of the Society's Gold Medal. Earlier this year I was prevailed upon by Council to prepare the Wright Brothers Lecture. This is an occupational hazard of the Director, RAE, and has led to a situation—unique in my experience—in which the Society has presented the Medal and then within a few minutes asked the recipient to stand up and earn it. I am not at all optimistic about the outcome—but will do my best.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1972 

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. Morgan, M. B. Supersonic aircraft—promise and problems. Journal of the Royal Aeronautical Society, June 1960.Google Scholar
2. Blackall, T. E. Concorde—the story, the facts and the figures. G. T. Foulis and Co Ltd, 1969.Google Scholar
3. Davis, J. The Concorde affair. Leslie Frewin Publishers Ltd, 1969.Google Scholar
4. Roy, M. Caracterès de l'ecoulement autour d'une aile en flèche accentuée. C. R. Acad Sci. (Paris) 234, 1952.Google Scholar
5. Legendre, R. Ecoulement au voisinage de la pointe avant d'une aile à forte flèche aux incidence moyennes. Rech Aero 30, 31 and 35, 1952-53.Google Scholar
6. Maskell, E. C. Flow separation in three dimensions. RAE Report Aero 2565, November 1955.Google Scholar
7. Maskell, E. C. and Kucheman, D. Controlled separation in aerodynamic design. RAE Technical Memorandum Aero 463, March 1956.Google Scholar
8. Maskell, E. C. and Weber, J. On the aerodynamic design of slender wings. RAE Report Aero 2610, August 1958. Also published in the Journal of the Royal Aeronautical Society, December 1959.Google Scholar
9. Lambourne, and Bryer, . Bursting of leading edge vortices—some observations and discussions of the phenomenon. RM 3282, April 1961.Google Scholar
10. Lawford, and Beavenham, . Low speed wind tunnel measurements on a thin sharp edged delta wing with 70° leading edge sweep, with particular reference to the position of the leading edge vortex breakdown. RM 3338, November 1961.Google Scholar
11. Earnshaw, and Lawford, . Low speed wind tunnel experiments on a series of sharp edged delta wings. RM 3424, March 1964.Google Scholar
12. Tomlinson, .and Wilcock, . Further piloted simulation studies of the handling characteristics of slender wing supersonic transport aircraft during approach and landing. RM 3660, 1969.Google Scholar
13. Neumark, S. Problems of longitudinal stability below minimum drag speed and theory of stability under constraint. RM 2983, 1953.Google Scholar
14. McKinney, and Drake, . Flight characteristics at low speeds of delta winged models. NACA TIB 1537, 1948.Google Scholar
15. Gray, W. E. Dynamic tests on free flying models of slender wings, subjected to side gusts. RM 3460, 1964.Google Scholar
16. Pinsker, W. J. The lateral motion of aircraft and in particular of inertially slender configurations. RM 3334, 1961.Google Scholar
17. Owen, . Low speed wind tunnel measurements of oscillatory rolling derivatives on a sharp edged slender wing effects of frequency parameter and of ground. RAE TR 68090, April 1968.Google Scholar
18. Pinsker, W. J. The aerodynamic effect of ground proximity on lateral control of slender aircraft in the landing approach. RAE TR 70079.Google Scholar
19. Wilde, M. G. and Cormery, G. The aerodynamic derivation of the Concorde wing. 11th Anglo-American Aeronautical Conference, Paper No 18. September 1969.Google Scholar