Author

Contributions

  • Stein, Manuel - Contributor
  • Schildcrout, Murry - Contributor
  • United States. National Advisory Committee for Aeronautics - Contributor
  • Langley Aeronautical Laboratory - Contributor

Publication

1947 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia

Language

English

Word Count

7,000 words, Guess

Page Count

28 pages

Identifiers

Classifications

  • DDC624.17762
  • LCCTA660.S5

Description

A theoretical solution is presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical curves and formulas for use in design. Comparisons are made with theoretical and empirical solutions obtained in other investigations.

Subjects

Series Statement

  • National Advisory Committee for Aeronautics technical note -- no. 1345
  • Technical note (United States. National Advisory Committee for Aeronautics) -- no. 1345.

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