Hostname: page-component-78c5997874-m6dg7 Total loading time: 0 Render date: 2024-11-19T11:41:53.930Z Has data issue: false hasContentIssue false
  • English
  • Français

Flutter and Stability

Published online by Cambridge University Press:  28 July 2016

W. J. Duncan
Get access Rights & Permissions [Opens in a new window]

Extract

The theme of flutter has not often been the subject of lectures before this Society, but the earliest of these was given as long ago as 1929 by my friend and former colleague Dr. R. A. Frazer. At that time a secure foundation for flutter theory had been laid and the principal methods for flutter prevention were already known. However, both theory and practice have developed much since 1929 and flutter has become of greater relative importance.

Type
Research Article
Information
The Aeronautical Journal , Volume 53 , Issue 462 , June 1949 , pp. 529 - 557
Copyright
Copyright © Royal Aeronautical Society 1949

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. Frazer, R. A. The flutter of aeroplane wings. Journal R.Ae.S., p. 407, June 1929.Google Scholar
2. Collar, A. R. The expanding domain of aeroelasticity. Journal R.Ae.S., p. 613. Aug. 1946.Google Scholar
3. Duncan, W. J. The fundamentals of flutter. Aircraft Engineering, vol. 17, pp. 16 and 32, Jan. and Feb. 1945. (To appear also as R. and M. 2417.)Google Scholar
4. Duncan, W. J. The representation of aircraft wings, tails and fuselages by semi-rigid structures in dynamic and static problems. R. and M. 1904. Feb. 1943.Google Scholar
5. Frazer, R. A. Interim note on a theoretical investigation of the influence of mass on wing flutter. A.R.C. 6720. May 1943.Google Scholar
6. Minhinnick, I. T. and Yarwood, J. Interim note on the theoretical effects of an engine mass on wing flutter. A.R.C. 6728. R.A.E. Tech. Note No. S.M.E. 143. May 1943.Google Scholar
7. Lambourne, N. C. and Weston, D. An experimental investigation of the effect of localised masses on the flutter and resonance of a model wing. A.R.C. 7604. April 1944.Google Scholar
8. Frazer, R. A. and Duncan, W. J. The flutter of monoplanes, biplanes and tail units. (A.R.C. Monograph.) R. and M. 1255. Jan. 1931.Google Scholar
9. Pugsley, A. G., Morris, J. and Naylor, G. A. The effect of fuselage mobility in roll upon wing flutter. R. and M. 2009. Oct. 1939.Google Scholar
10. Duncan, W. J. Flutter of systems with many freedoms. College of Aeronautics Report No. 19. Aug. 1948.Google Scholar
11. Küssner, H. G. Schwingungen von Flugzeugflügeln. Luftfahrtforschung, vol. 4, p. 41. June 1929.Google Scholar
12. Pugsley, A. G. A simplified theory of wing flutter. R. and M. 1839. April 1937.Google Scholar
13. Duncan, W. J. and Lyon, H. M. Calculated flexural-torsional flutter characteristics of some typical cantilever wings. R. and M. 1782. April 1937.Google Scholar
14. Duncan, W. J. and Griffith, C. L. T. The influence of wing taper on the flutter of cantilever wings. R. and M. 1869. 1939.Google Scholar
15. Pugsley, A. G. The influence of wing density upon the flutter of aeroplane wings. R. and M. 1497. June 1932.Google Scholar
16. Duncan, W. J. and Collar, A. R. The present position of the investigation of airscrew flutter. R. and M. 1518. Dec. 1932.Google Scholar
17. Frazer, R. A. and Jones, W. P. Wing-ailerontab flutter (Parts I and II). A.R.C. 5668. Mar. 1942.Google Scholar
18. Collar, A. R. The prevention of flutter of spring-tabs. R. and M. 2034. May 1943.Google Scholar
19. Collar, A. R. and Sharpe, G. D. Mass-balance for spring tab flutter prevention. A.R.C. 9104. R.A.E. Report No. S.M.E. 3346. Oct. 1945.Google Scholar
20. Baumhauer, A. G. Von and Koning, C. On the stability of oscillations of an aeroplane wing. International Air Congress 1923. Report, p. 221.Google Scholar
21. Bryan, G. H. Stability in Aviation. Macmillan, London, 1911.Google Scholar
22. Duncan, W. J. Some notes on aerodynamic derivatives. R. and M. 2115. April 1945.Google Scholar
23. Frazer, R. A. and Duncan, W. J. The flutter of aeroplane wings. (A.R.C. Monograph.) R. and M. 1155. Aug. 1928.Google Scholar
24. Bratt, J. B. and Wight, K. C. The effect of mean incidence, amplitude of oscillation, profile and aspect ratio on pitching moment derivatives. R. and M. 2064. June 1945.Google Scholar
25. Glauert, H. The force and moment on an oscillating aerofoil. R. and M. 1242. Mar. 1929.Google Scholar
26. Wagner, H. Uber die entstehung des dynamischen Auftriebes von Tragflügeln. Z.A.M.M., vol. 5, p. 17. 1925.Google Scholar
27. Duncan, W. J. and Collar, A. R. Resistance derivatives of flutter theory. R. and M. 1500. Oct. 1932.Google Scholar
28. Theodorsen, T. General theory of aerodynamic instability and the mechanism of flutter. N.A.C.A. Report 496. 1935.Google Scholar
29. Küssner, H. G. Augenblicklicher Entwicklungstand del Frage des Flügelflatterns. Luftfahrtforschung, vol. 12, p. 193. Oct. 1935.Google Scholar
30. Cicala, P. Le azioni aerodinamiche sul profilo oscillante. L'Aerotecnica, vol. 16, p. 653. 1936.Google Scholar
31. Possio, C. L'azione aerodinamica sul profilo oscillante in un fluido compressibile a velocita iposonora. L'Aerotecnica, vol. 18, p. 441. 1938.Google Scholar
32. Frazer, R. A. Possio's derivative theory for an infinite aerofoil moving at subsonic speeds. A.R.C. 4932. Jan. 1941.Google Scholar
33. Dietze, F. Die Luftkrafte des harmonisch schwingenden Flügels in kompressiblen Medium bei Unterschallgeschwindigkeits. R.T.P. Translation 1317. A.R.C. 5440.Google Scholar
34. Borbely, S. Von. Ueber die Luftkrafte, die auf einen harmonisch schwingenden zweidimensionalen Flügel bei Uberschallgeschwindigkeit wirken. Z.A.M.M., vol. 22, p. 190. 1942.Google Scholar
35. Temple, G. and Jahn, H. A. Flutter at supersonic speeds. Part I. Mid-chord derivative coefficients for a thin aerofoil at zero incidence. R. and M. 2140. April 1945.Google Scholar
36. Bratt, J. B. and Chinneck, A. Measurement of mid-chord pitching moment derivatives at high speeds. A.R.C 10,709. June 1947.Google Scholar
37. Lyon, H. M. Aerodynamical derivatives of flexural-torsional flutter of a wing of finite span. A.R.C. 2999. May 1937.Google Scholar
38. Cicala, P. Theory and experiments on the phenomenon of wing vibration. Translated from L'Aerotecnica, vol. 18, April 1938. (A.R.C. 3800.)Google Scholar
39. Jones, W. P. Aerodynamic forces on wings in simple harmonic motion. R. and M. 2026. Feb. 1945.Google Scholar
40. Jones, W. P. Theoretical air-load and derivative coefficients for rectangular wings. R. and M. 2142. Feb. 1943.Google Scholar
41. Schwarz, L. A semi-experimental method for determining unsteady pressure distributions. A.R.C. 10,387. Feb. 1947.Google Scholar
42. Jones, W. P. Aerofoil oscillations at high mean incidences. A.R.C. 11,502. April 1948.Google Scholar
43. Duncan, W. J. Note on the best choice of reference section for semi-rigid wings. A.R.C. 5833. May 1942.Google Scholar
44. Victory, M. Choice of reference section for calculation of flutter speeds of semi-rigid wings. A.R.C. 6143. R.A.E. Report No. S.M.E. 3228. Sept. 1942.Google Scholar
45. Duncan, W. J., Collar, A. R. and Lyon, H. M. Oscillations of elastic blades and wings in an airstream. R. and M. 1716. Jan. 1936.Google Scholar
46. Roxbee Cox, H. A statistical method of investigating the relations between the elastic stiffnesses of wings and wing-aileron flutter. R. and M. 1505. Oct. 1932.Google Scholar
47. Collar, A. R., Broadbent, E. G. and Puttick, E. B. An elaboration of the criterion for wing torsional stiffness. R. and M. 2154. Jan. 1946.Google Scholar
48. Southwell, R. V. Unpublished communication to the Flutter Sub-Committee of the A.R.C. 1927. See also Ref. No. 23.Google Scholar
49. Frazer, R. A., Duncan, W. J. and Collar, A. R. Elementary Matrices. Cambridge University Press, 1938.Google Scholar
50. Schlippe, B. Von. Zur Frage der selbsterregten Flügelschwingungen. Luftfahrtforschung, vol. 13, p. 41. 1936.Google Scholar
51. Frazer, R. A. and Jones, W. P. Forced oscillations of aeroplanes, with special reference to von Schlippe's method of predicting critical flutter speeds. R. and M. 1795. 1937.Google Scholar
52. Duncan, W. J. Mechanical admittances and their applications to oscillation problems. (A.R.C. Monograph.) R. and M. 2000. Mar. 1946.Google Scholar
53. Duncan, W. J. The principles of the Galerkin method. R. and M. 1848. Sept. 1938.Google Scholar
54. Duncan, W. J. Ignoration of distortional coordinates in the theory of stability and control. Report No. 1 of the College of Aeronautics, Cranfield. Dec. 1946.Google Scholar
55. Gates, S. B. and Lyon, H. M. A continuation of longitudinal stability and control analysis. Part I. General theory. R. and M. 2027. Feb. 1944. Part II. Interpretation of flight tests. R and M. 2028. Aug. 1944.Google Scholar
56. Bratt, J. B., Wight, K. C. and Tilly, V. J. The application of a “Wattmeter” Harmonic Analyser to the measurement of aerodynamic damping for pitching oscillations. R. and M. 2063. May 1942.Google Scholar
57. Bratt, J. B., Raymer, W. G. and Miles, C. J. W. Interim note on the measurement of torsional derivatives in the compressed air tunnel. A.R.C. 6339. Dec. 1942.Google Scholar
58. Milliken, W. F. Progress in dynamic stability and control research. Journal Aero. Sci, vol. 14, p. 493. Sept. 1947.Google Scholar
59. Smilg, B. The prevention of aileron oscillations at transonic speeds. Sixth International Congress of Applied Mechanics, Paris, 1946.Google Scholar
60. Lyons, D. J. Present thoughts on the use of power flying controls in aircraft. Journal R.Ae.S. Dec. 1948.Google Scholar
61. Jahn, H. A., Buxton, G. H. L., and Minhinnick, I. T. Fuselage vertical bending—elevator flutter on the Typhoon. R. and M. 2121. Mar. 1944.Google Scholar
62. Collar, A. R. and Grinsted, F. The effects of structural flexibility of tailplane, elevator and fuselage on longitudinal stability and control. R. and M. 2010. Sept. 1942.Google Scholar
63. Studer, H. L. Experimental investigation of wing flutter. (Translation by W. J. Stern.) A.R.C. 2777. 1936.Google Scholar
64. Victory, M. Flutter at high incidence. R. and M. 2048. Jan. 1943.Google Scholar
65. Lambourne, N. C. An experimental investigation on a model flying wing. A.R.C. 10,509. April 1947.Google Scholar
66. Shaw, R. A. Changes in control characteristics with changes in flow pattern at high subsonic speeds. Tests on an E.C.1250 Aerofoil with 25 per cent, concave control flap. A.R.C. 11,933. Nov. 1948.Google Scholar
67. Mitchell, K. Lateral response theory. A.R.C. 7993. R.A.E. Report No. Aero 1925. Mar. 1944.Google Scholar
68. Duncan, W. J. Tail buffeting. Journal R.Ae.S. p. 108. Feb. 1934.Google Scholar
69. Williams, J. The experimental determination of airloads on oscillating aerofoil systems. A.R.C. 11,715, Aug. 1948, M.O.S. TIB/MISC/ 833.Google Scholar
70. Williams, J. Applied investigations on aircraft flutter. A.R.C. 11,716. Aug. 1948. M.O.S. TIB/ MISC/832.Google Scholar
71. Williams, J. General methods for the investigation of aircraft flutter. A.R.C. 11,717. Aug. 1948. M.O.S. TIB/MISC/838.Google Scholar
72. Williams, J. A bibliography of researches on the aerodynamic theory of wings in nonuniform motion. A.R.C. 11,718. Aug. 1948. M.O.S. TIB/MISC/859.Google Scholar