Column Stability

Compression strengths of columns can be predicted using theoretical elastic solutions for slender, symmetrical and centroidally-loaded columns. For short or eccentrically loaded columns, corrections need to be made using one of several methods:

  • non-linear material behavior for compact sections

  • semi-empirical method based on test data

  • a curve fit (interaction) from Euler solution to cutoff (crippling, yield) such as Johnson-Euler.

Note: Beam-column strength checks should be done, even on symmetrically loaded columns, with an assumed manufacturing tolerance such as L/400.

Column Properties Input


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Section Properties





Length and Fixity




Material Properties

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Applied Load (optional)


M.S. Labeling (FS ONLY USED WHEN LIMIT LOAD SELECTED)







References

Timoshenko, S. P., and Gere, J. M. (1961). Theory of Elastic Stability (2nd ed.). McGraw-Hill, New York, NY. Euler buckling, end-fixity coefficients, columns under distributed axial load.

Bruhn, E. F. (1973). Analysis and Design of Flight Vehicle Structures. Tri-State Offset Company, Cincinnati, OH. Chapter C2, column strength: tangent-modulus (Euler-Engesser) and Johnson-Euler methods.

Ramberg, W., and Osgood, W. R. (1943). Description of Stress-Strain Curves by Three Parameters. NACA Technical Note 902. Stress-strain curve used for the tangent modulus.

Boresi, A. P., and Schmidt, R. J. (2003). Advanced Mechanics of Materials (6th ed.). John Wiley & Sons, Hoboken, NJ. Principal second moments of area.

Niu, M. C. Y. (2001). Airframe Stress Analysis and Sizing (2nd ed.). Hong Kong Conmilit Press, Hong Kong. Column and crippling allowables.

MIL-HDBK-5J (2003). Metallic Materials and Elements for Aerospace Vehicle Structures. U.S. Department of Defense. Material allowables filled by the dropdown.


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