Author

Contributions

  • Mayers, J. - Contributor
  • United States. National Advisory Committee for Aeronautics - Contributor

Publication

1952 - National Advisory Committee for Aeronautics, Washington, D.C, Ohio

Language

English

Word Count

8,500 words, Guess

Page Count

34 pages

Identifiers

Classifications

  • DDC624.17765
  • LCCTA660.P6

Description

Theoretical solutions are presented for the buckling in uniform axial compression of two types of simply supported curved sandwich plates: the corrugated-core type and the isotropic type. Results are given in the form of equations and curves.

Subjects

Series Statement

  • National Advisory Committee for Aeronautics -- no. 2601
  • Technical note (United States. National Advisory Committee for Aeronautics) -- no. 2601.

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