Hostname: page-component-848d4c4894-pjpqr Total loading time: 0 Render date: 2024-07-03T08:53:15.766Z Has data issue: false hasContentIssue false
  • English
  • Français

Instability of Monocoque Structures in Pure Bending

Published online by Cambridge University Press:  28 July 2016

N. J. Hoff
Get access Rights & Permissions [Opens in a new window]

Extract

The growing demand for aerodynamically advantageous forms, for smooth surfaces, and last but not least for a better ratio of useful cross section to total cross section of fuselages lead to an increasing application of monocoque structures in aircraft construction. Unlike ordinary beams the behaviour of such thin walled structures under loads and their ultimate failure is influenced a great deal by instability phenomena. In the present paper these problems are dealt with in some detail for the case of pure bending.

Type
Research Article
Information
The Aeronautical Journal , Volume 42 , Issue 328 , April 1938 , pp. 291 - 346
Copyright
Copyright © Royal Aeronautical Society 1938

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

List of References

1. The flexure of thin cylindrical shells and other “thin” sections. By L. G. Brazier, . A.R.C. Rep. and Mem. No. 1081, 1927.Google Scholar
2. Buckling of thin plates in compression. By H. L. Cox, . A.R.C. Rep. and Mem. No. 1554, 1933.Google Scholar
3. Die Druckfestigkeit versteifter zylindrischer Schalen. By Dji-Djüän Dschou, . Luftfahrt-forschung, Vol. XI, Issue 8, 1935.Google Scholar
4. Theorie und Versuche zur Festigkeit von Schalenrumpfen. By H. Ebner, . Luftfahrtforschung, Vol. XIV, Issue 3, 1937.Google Scholar
5. Drang und Zwang. By A. & L. Föppl. Oldenbourg, München und Berlin, 1924.Google Scholar
6. Monocoque construction. By Gerard, I. J. The Journal of the Royal Aeronautical Society, June, 1937.Google Scholar
7. Ueber die Stabilität orthotroper elliptischer Zylinderschalen bei reiner Biegung. By Heck, O. S. Luftfahrtforschung, Vol. XIV, Issue 3, 1937.Google Scholar
8. Elastically encastred struts. By Hoff, N. J. The Journal of the Royal Aeronautical Society, September, 1936.Google Scholar
9. Formulæ and methods of calculation of the strength of plate and shell structures in aeroplane construction. By Heck, O. S. and Ebner, H. The Journal of the Royal Aeronautical Society, October, 1936.Google Scholar
10. The strength of thin plates in compression. By Kármán, Th. von. Calif. Inst, of Techn., Pasadena, Publication No. 13, 1932.Google Scholar
11. Ueber die Formänderung dünnwandiger Rohre, insbesondere federnder Ausgleichsrohre. By Th. von Kármán, . Zeitschrift des Vereins Deutscher Ingenieure. Vol. LV, p. 1889, 1911.Google Scholar
12. Aerodynamic and structural features of tapered wings. By Lachmann, G. V. The Journal of the Royal Aeronautical Society, March, 1937.Google Scholar
13. Versuche zur Ermittlung der mittragenden Breite von verbeulten Blechen. By Lahde, R. and Wagner, H. Luftfahrtforschung, Vol. XIII, Issue 7, 1936.Google Scholar
14. Comparison of three methods for calculating the compressive strength of flat and slightly curved sheet and stiffener combinations. By Eugene E. Lundquist. N.A.C.A. Techn. Note No. 455, 1933.Google Scholar
15. Strength tests of thin-walled duralumin cylinders in pure bending. By Eugene E. Lundquist. N.A.C.A. Techn. Note No. 479. 1933.Google Scholar
16. Die mittragende Breite der gedrückten Platte. By K. Marguerre, . Luftfahrtforschung, Vol. XIV, Issue 3, 1937.Google Scholar
17. Die mittragende Breite. By Metzer, W. Luftfahrtforschung, Vol. IV, Issue 1, 1929.Google Scholar
18. Aeroplane structures. By Sutton Pippard, A. J. and Laurence Pritchard, J. Longman's, Green & Co., London, 1935.Google Scholar
19. Elastic instability of a thin curved panel. By Redshaw, S. C. A.R.C. Rep. and Mem. No. 1565, 1933.Google Scholar
20. Appendix to Ref. 10. By Ernest E. Sechler and L. H. Donnell.Google Scholar
21. Strength of rectangular flat plates under edge compression. By Shuman, L. and Back, G. N.A.C.A. Rep. No. 356.Google Scholar
22. Theory of elastic stability. By Timoshenko, S. MacGraw-Hill Book Co., New York and London, 1936.Google Scholar
23. Notes on the strength of stressed skin fuselages. By Wallace, G. F. The Journal of the Royal Aeronautical Society, April, 1936.Google Scholar