Hostname: page-component-848d4c4894-jbqgn Total loading time: 0 Render date: 2024-06-19T19:38:13.360Z Has data issue: false hasContentIssue false

Aerodynamic Design

Published online by Cambridge University Press:  04 July 2016

D. Küchemann*
Affiliation:
Royal Aircraft Establishment

Extract

I am very conscious of the great honour of being invited to deliver this fourth Reynolds-Prandtl Lecture. At the same time, I am very pleased. As far as I am concerned, the spirit of these two great scientists is still alive. They are both with me every day—at least, I have pictures of them in my office and I look at them every day. As has been said before, their influence is as strong as ever and many of the problems that engaged their attention are even today only partially solved. However, there is more to it than that. Their example and their work have left me with many other problems to think about, which concern the kind of work we do and the aims we pursue. The present lecture gives me an opportunity to put before you some of the thoughts that occupy my mind and which I should like to be discussed. I feel quite strongly that these problems deserve our attention. It may even be vital for the survival of research in our field to find answers to them, which satisfy not only ourselves but also the society in which we live.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1969 

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. Reynolds, O. Papers on Mechanical and Physical Subjects. 3 volumes. Cambridge University Press, 1900, 1901, and 1903.Google Scholar
2. Lamb, H. Osborne Reynolds, 1842 to 1912. Biographical Memoir Proc Roy Soc (A), Vol 88, No XV, 1913.Google Scholar
3. Prandtl, L. Gesammelte Abhandlungen zur angewandten Mechanik, Hydro-und Aerodynamic. 3 volumes. Springer, 1961.Google Scholar
4. Busemann, A. Ludwig Prandtl, 1875-1953, Biographical Memoirs of Fellows of the Royal Society, Vol 5, 1960.Google Scholar
5. Taylor, G. I. Scientific methods in aeronautics. The Wilbur Wright Lecture, 1921. Journal of the Royal Aeronautical Society, Vol 25, No 474, 1921.Google Scholar
6. Popper, K. R. Conjectures and Refutations. The Growth of Scientific Knowledge. Routledge & Kegan Paul, 1963.Google Scholar
7. Motycka, D. L., Skowronek, P. J. Jr. Use of statistically designed experiments in wind-tunnel test programmes. Jour Aircraft, Vol 4, No 297, 1967.Google Scholar
8. Cockburn, Sir Robert. A new phase in Aviation? 56th Wilbur and Orville Wright Memorial Lecture, 1967. Journal of the Royal Aeronautical Society, Vol 72, pp 199208, March 1968.Google Scholar
9. Lanchester, F. W. The Flying Machine. Inst Automobile Engineers, 1915.Google Scholar
10. Medawar, P. B. The Art of the Soluble. Methuen, 1967.Google Scholar
11. Maskell, E. C. On the principles of aerodynamic design. Progr in Aeron Sci, Vol 1, No 1, 1961.Google Scholar
12. Maskell, E. C., Weber, J. On the aerodynamic design of slender wings. Journal of the Royal Aeronautical Society, Vol 63, No 709, 1959.Google Scholar
13. Küchemann, D., Weber, J. An analysis of some performance aspects of various types of aircraft designed to fly over different ranges at different speeds. Progr in Aeron Sci, Vol 9, No 329, 1968.Google Scholar
14. Küchemann, D. Hypersonic aircraft and their aerodynamic problems. Progr in Aeron Sci, Vol 6, No 271, 1965. See also: Hyperschallflugzeuge und ihre aerodynamischen Probleme. p 85, WGLR, Jahrb 1964.Google Scholar
15. Küchemann, D. An aerodynamicist's prospect of the Second Century. Journal of the Royal Aeronautical Society, Vol 72, pp 109114, February 1968.Google Scholar
16. Küchemann, D. Die aerodynamische Entwicklung von schlanken Flügeln für den Überschallflug. p 66, WGLR, Jahrb 1962. See also: Slender wings for supersonic flight. Shell Aviation News, No 294, p 14 and No 295, p 14, 1962.Google Scholar
17. Hummel, D. Untersuchungen über das Aufplatzen der Wirbel an schlanken Deltaflügeln. Zeitschr Flugwiss, Vol 13, No 158, 1965.Google Scholar
18. Hall, M. G. The structure of concentrated vortex cores. Progr in Aeron Sci, Vol 7, No 53, 1966.Google Scholar
19. Ross, A. J. The lateral oscillation of slender aircraft. Unpublished MOA Report.Google Scholar
20. Pinsker, W. J. G. Features of large transport aircraft affecting control during approach and landing. AGARD Report No. 421, January 1963.Google Scholar
21. Bagley, J. A. Some aerodynamic principles for the design of swept wings. Progr in Aeron Sci, Vol 3, No 1, 1962.Google Scholar
22. Küchemann, D. Inviscid shear flow near the trailing edge of an aerofoil. Zeitschr Flugwiss, Vol 15, No 292, 1967.Google Scholar
23. Williams, J., Ross, A. J. Some airframe aerodynamic problems at low speeds. Proc Int Congr of Subsonic Aerod, New York Acad Sci, 1967.Google Scholar
24. Wimpenny, J. C. The design and application of high lift devices. Proc Int Congr of Subsonic Aerod, New York Acad Sci, 1967.Google Scholar
25. Küchemann, D., Weber, J. Aerodynamics of Propulsion. McGraw-Hill, 1953.Google Scholar
26. European Mechanics Colloquia. Journ Fluid Mech, Vol 29, part 4, September 1967; Journal of the Royal Aeronautical Society, Vol 71, p LXII, September 1967; VDI Nachr Nr 38, September 1967.Google Scholar