Summary
The critical load of a structure is that load at which elastic buckling occurs. In this paper, the critical load of lateral buckling of a single triangle is evaluated, the assumption being made that the joints are fixed in position in space but free to rotate. The use of matrix algebra greatly simplifies the problem.
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Abbreviations
- c AB :
-
carryover factor, tabulated in ref. 5)
- C AB :
-
torsional carryover factor from end A to end B of member AB
- D /1 A :
-
displacement matrix at joint A, referred to the coordinate axes of the framework
- F /1 A :
-
force matrix at joint A, referred to framework axes
- E :
-
Young's modulus
- I :
-
2nd moment of area about the axis of bending
- k :
-
EI/L
- L :
-
length of the member
- M A :
-
moment at joint A
- M AB :
-
moment at joint A in member AB
- s AB :
-
stiffness factor in bending at end A in member AB, tabulated in ref. 5)
- S AB :
-
torsional stiffness at end A of member AB
- T :
-
transformation matrix, to convert from the coordinate axes of the member to the coordinate axes of the framework
- T AB :
-
torque at end A in member AB
- Y AB :
-
stiffness matrix of end A member AB, referred to member axes
- Y /1 AB :
-
stiffness matrix of end A member AB, referred to framework axes
- Y /1 ABB :
-
carryover matrix from end A to end B in member AB referred to framework axes
- Y /1 BAA :
-
carryover matrix from end B to end A in member AB, referred to framework axes
- α :
-
angles of the frame measured in the plane of the frame
- γ AB :
-
twist of end A of member AB caused by torque T AB
- θ AB :
-
rotation of end A of member AB caused by moment M AB
References
Hoff, N. J., J. Roy Aero. Soc. 45 (1941) 241.
Winter, G., R. T. Hsu, B. Koo and M. H. Loh, Bull No. 36 Apr. 1948, Cornell University, Ithaca, New York.
Bolton, A., J. Inst. Struct. Engrs 33 (1955) 90.
Allen, H. G., Proc. Roy. Soc. A231 (1955) 25.
Livesley, R. K. and D. B. Chandler, Stability Functions of Structural Frameworks, Manchester Univ. Press 1956.
Livesley, R. K., Engineering 176 (1953) 230.
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Nutt, J.G. The critical load of a triangular framework when lateral buckling occurs. Appl. sci. Res. 8, 169–176 (1959). https://doi.org/10.1007/BF00411747
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DOI: https://doi.org/10.1007/BF00411747