Author

Contributions

  • Becker, Herbert, 1918- - Contributor
  • United States. National Advisory Committee for Aeronautics - Contributor

Publication

1957 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia

Language

English

Word Count

38,500 words, Guess

Page Count

154 pages

Identifiers

Classifications

  • DDC623.817
  • LCCTA645

Description

Available theories and test data on buckling of curved plates and shells are reviewed. For torsion and external-pressure loadings, the test data are correlated in terms of linear buckling theories for both the elastic and inelastic ranges. The cases which exhibit a marked disagreement between linear theory and test data include those of curved plates and cylinders under axial compression, cylinders under bending, and spherical plates under external pressure. These cases have been analyzed by a unified semiempirical approach for both the elastic and inelastic ranges which is satisfactory for analysis and design purposes. The effects of internal pressure on buckling of elements under uniaxial loads are discussed and data on various combined loadings are presented in interaction form.

Subjects

Series Statement

  • Technical note / National Advisory Committee for Aeronautics -- 3783
  • Technical note (United States. National Advisory Committee for Aeronautics) -- no. 3783.

Links

Other Editions

  • Handbook of structural stabilityNational Advisory Committee for Aeronautics1957

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