Hostname: page-component-78c5997874-94fs2 Total loading time: 0 Render date: 2024-11-05T10:07:20.567Z Has data issue: false hasContentIssue false
  • English
  • Français

The Domain of the Helicopter

Published online by Cambridge University Press:  28 July 2016

Raoul Hafner
Get access Rights & Permissions [Opens in a new window]

Extract

When accepting the invitation to present the Seventh Louis Blèriot Memorial lecture, the author was deeply conscious not only of the honour which was bestowed upon him by this invitation but, in an equal measure, of the responsibility which attached to it.

For the first time one of the eminent memorial lectures is devoted to the rotating wing; the helicopter has been raised to the level of discussion of the great aeronautical papers.

The natural impulse of the gentler sex when faced with a great occasion is invariably: “how shall one dress?” To the author, a somewhat similar problem became manifest: how can the helicopter, this new-comer, best be “ dressed?” How should it be presented, so as to make not only a good impression but also a full and, above all, a true impression?

Type
Research Article
Information
The Aeronautical Journal , Volume 58 , Issue 526 , October 1954 , pp. 663 - 702
Copyright
Copyright © Royal Aeronautical Society 1954

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. Leonardo, Da vinci. Codex B fol. 83.v.Google Scholar
2. Chanute, O. (1894). Progress in Flying Machines (1894).Google Scholar
3. Royal Aeronautical Society (1896). Correspondence (1896).Google Scholar
4. Lame, M. L. V. Le Vol Vertical. Thèorie Gènèrate de l'Hèlicoptère. Les Appareils aux Voilures Tournantes de Leur Origine à 1934.Google Scholar
5. Juan, De la Cierva (1935). New Developments of the Autogyro. Journal of the Royal Aeronautical Society. December 1935.Google Scholar
6. Federation Aéronautique Internationale. Records Offlciels Homologués au 31 Décembre 1953.Google Scholar
7. Final Report of the Daniel Guggenheim International Safe Aircraft Competition. January 1930.Google Scholar
8. Handley Page, F. (1950): Towards Slower and Safer Flying, Improved Take-off and Landing, and Cheaper Airports. The Third Louis Bleriot Lecture. May 1950. Journal of the Royal Aeronautical Society. Dec. 1950.Google Scholar
9. International Air Transport Association. A Condensed Record of the Symposium on the Operation and Design Requirements of Helicopters, held during the Sixth Annual Technical Conference of I.A.T.A. at Puerto Rico in April 1953. Doc. Gen. 135/ (1953).Google Scholar
10. Daniel, De foe (about 1700).Google Scholar
11. Oxford English Dictionary. Third Edition.Google Scholar
12. Glauert, H. (1926). A General Theory of the Autogyro. A.R.C. R. & M. 1111 (1926).Google Scholar
13. Lock, C. N. H. (1927). Further Development of Auto gyro Theory. A.R.C. R. & M. 1127 (1927).Google Scholar
14. Hafner, R. (1938). The Hafner Gyroplane. Royal Aeronautical Society, October 1937. Journal of the Royal Aeronautical Society. February 1938.Google Scholar
15. NIKOLSKY, A. A. (1951). Helicopter Analysis. J. Wiley, New York (1951).Google Scholar
16. Hafner, R. (1948). The Bristol 171 Helicopter. Royal Aeronautical Society, November 1948. Journal of the Royal Aeronautical Society. April 1949.Google Scholar
17. Hafner, R. (1947). Rotor Systems and Control Problems in the Helicopter. First Anglo-American Aeronautical Conference, September 1947. Royal Aeronautical Society 1948.Google Scholar
18. Berggren, R. E. and Graham, D. J. (1950). Effects of Leading-edge Radius and Maximum Thickness-chord Ratio on the Variation with Mach Number of the Aero dynamic Characteristics of Several Thin N.A.C.A. Airfoil Sections. N.A.C.A. R.M. A.50D04 (July 1950). N.A.C.A. T.I.B.2413.Google Scholar
19. Laitone, E. V. and Talbot, L. (1953). Subsonic Com pressibility Corrections for Propellers and Helicopter Rotors. Journal of the Aeronautical Sciences. October 1953.Google Scholar
20. Lock, C. N. H., Bateman, H. and Townend, H. C. H. (1926). An Extension of the Vortex Theory of Airscrews. R. & M. 1014 (June 1926).Google Scholar
21. Fitzwilliams, O. L. L. (1951). The Giant Helicopter. Royal Aeronautical Society, November 1951. Journal Helicopter Association of Great Britain,.Vol. 5, No. 4, 1952.Google Scholar
22. Nickols, J. B. (1953). Tip-mounted Turbojet Engines for Helicopter Rotor Propulsion. American Helicopter Society. Ninth Annual Forum. May 1953.Google Scholar
23. Herrick, G. P. (1938). The Convertaplane. Institute of the Aeronautical Sciences, Philadelphia. October 1938.Google Scholar
24. Proceedings of the First Convertible Aircraft Congress, Philadelphia. 1949.Google Scholar
25. Proceedings of the Second Convertible Aircraft Congress, Philadelphia. 1952.Google Scholar
26. Masefield, P. G. (1948). Some Economic Factors in Civil Aviation. Fourth British Commonwealth and Empire Lecture. Journal of the Royal Aeronautical Society. October 1948.Google Scholar
27. Weichsel, H. (1953). Several Considerations derived from Commercial Helicopter Sales Experience. Proceed ings of the St. Louis, Missouri Section of I.A.S. and A.H.S. November 1953. 10.Google Scholar
28. British European Airways. Outline Specification of Requirements for a Large Helicopter. October 1951, amended May 1952.Google Scholar
29. Society of British Aircraft Constructors. Standard Method for the Estimation of Direct Operating Costs of Aircraft. Issue No. 2, January 1953.Google Scholar
30. British European Airways. Report and Accounts. 1952- 1953.Google Scholar
31. Masefield, P. G. (1952). Some Thoughts on the Oper ational Future of the Transport Helicopter. Journal Helicopter Association of Great Britain, Vol. 6, No. 3. 1953.Google Scholar
32. Bernard Lafont.Google Scholar
33. Tobin, P. A. (1953). Development of the Helicopter. Journal of the Royal United Service Institution. November 1953.Google Scholar