Hostname: page-component-77c89778f8-swr86 Total loading time: 0 Render date: 2024-07-22T05:19:56.834Z Has data issue: false hasContentIssue false
  • English
  • Français

The Application of the Theory of Stability in Structural Design

Published online by Cambridge University Press:  04 July 2016

H. L. Cox
H. L. Cox*
Affiliation:
National Physical Laboratory
Get access Rights & Permissions [Opens in a new window]

Extract

It is never satisfactory to design a structure piecemeal. The whole construction ought to be considered as one unit and designed from the outset to meet each of the several loading actions to which it may be subjected. Part structures designed for one principal loading system and later modified to accord with other part structures or to meet other loading requirements, will seldom prove efficient. Moreover a structure designed from the outset to meet alternative loading cases is necessarily better integrated than a structure designed primarily for one loading case and later modified to meet another.

Type
Research Article
Information
The Aeronautical Journal , Volume 62 , Issue 571 , July 1958 , pp. 497 - 519
Copyright
Copyright © Royal Aeronautical Society 1958

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.Seide, P. and Barrett, P. F. (1951). The Stability of the Compression Cover of Box Beams Stiffened by Posts. N.A.C.A. Report No. 1047, 1951.Google Scholar
2.Cox, H. L. and Smith, H. E. (1943). Structures of Minimum Weight. A.R.C. R. & M. No. 1923, 1943.Google Scholar
3.Timoshenko, S. (1936). The Theory of Elastic Stability. McGraw-Hill Book Co., 1st Edition, p. 371, 1936.Google Scholar
4.Catchpole, E. J. (1954). The Optimum Design of Compression Surfaces having Unflanged Integral Stiffeners. Journal of the Royal Aeronautical Society, Vol. 58, p. 765, November 1954.Google Scholar
5.Farrar, D. J. (1949). The Design of Compression Struc tures for Minimum Weight. Journal of the Royal Aeronautical Society, Vol. 53, p. 1041, November 1949.Google Scholar
6.Anderson, R. A., Pride, R. A. and Johnson, A. E., Jnr. (1953). Some Information on the Strength of Thick-skin Wings with Multiweb and Multipost Stabilization. N.A.C.A. RM L.53 F.16 (NACA/TIB/3724), 1953.Google Scholar
7.Anderson, R. A. and Semonian, J. W. (1954). Charts Relating the Compressive Buckling Stress of Longitudinally Supported Plates to the Effective Deflectional and Rotational Stiffness of the Supports. N.A.C.A. Report No. 1202, 1954.Google Scholar
8.Semonian, J. W. and Peterson, J. P. (1956). An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-Stringer Panels with Special Reference to the Influence of the Riveted Connection between Sheet and Stringer. N.A.C.A. Report No. 1255, 1956.Google Scholar
9.Dow, Norris F., Ross Leven, L. and Troutman, J. L. (1953). Elastic Buckling under Combined Stresses of Flat Plates with Integral Waffle-Like Stiffening. N.A.C.A. T.N. 3059, October 1953.Google Scholar