Discussion
Letter to the Editor: Closure to discussion on the article ‘‘Rigid
body concept for geometric nonlinear analysis of 3D frames, plates
and shells based on the updated Lagrangian formulation’’ by
Y.B. Yang, S.P. Lin, C.S. Chen [Comput. Methods Appl. Mech.
Engrg. 196 (2007) 1178–1192]
Y.B. Yang
*, S.P. Lin, C.S. Chen
Department of Civil Engineering, National Taiwan University, Taipei 10617, Taiwan Received 3 July 2007; accepted 31 July 2007
Available online 14 September 2007
The discusser raises a very interesting question in the nonlinear analysis of three-dimensional framed structures, with regard to the appearance of the factor 1/2 for bisym-metric solid cross sections in Eq. (15), which relates to the rotational properties of internal moments. This is not an issue for the geometric nonlinear analysis of framed struc-tures using the approach presented in the paper for the fol-lowing reasons:
(1) The factor 1/2 in Eq. (15) arises from the adoption of the equality in Eq. (5.5.48) of Yang and Kuo [4], which is mathematically correct, as was noted by the discusser.
(2) In the nonlinear analysis of framed structures, distinc-tion should be made between the ‘‘internal moments’’, which are generated as the stress resultants over the cross section, and the ‘‘external moments’’, which are generated by external mechanical devices. With regard to the rotational properties of the internal tor-sion, one needs to know the composition of shear stresses sxyand sxzover a cross section, which cannot be determined solely from the sectional shape, and are not known before the problem is solved. For I-sec-tions, rather than for bisymmetrical solid secI-sec-tions, the parameter a cannot be directly related to Iy/Izin the way used by the discusser. See Yang and McGuire
[6]for a more general definition of a for I-sections.
(3) In contrast, we can always specify the rotational properties of external moments because they are gen-erated by external agencies.
(4) For a nonlinear structure to be in equilibrium, we can ‘‘cut’’ the structure into a number of ‘‘elements’’ (members) and ‘‘joints’’, and require each element and joint to be in equilibrium in the deformed state. The rotational components of internal moments on both sides of each ‘‘cut’’ will cancel out by themselves in the deformed state, as was stated in Section 5 of the paper or Sections 6.3 and 6.7 of Yang and Kuo[4], regardless of whether they are defined as semitangen-tial moments [1], generalized moments [2], or the one including the a parameter mentioned by the discusser. In other words, in the nonlinear analysis of three-dimensional frames, if a rational approach is adopted, the definition of the internal moments is really up to the choice of the researchers.
(5) The other difficulty encountered in defining the rotational properties of internal torsions is that they are not generally known before the solution is obtained. For instance, let us consider an I-beam subjected to an end torque. Depending on the extent of warping restraint at the two ends, which is unknown if the I-beam is part of a three-dimensional frame, the torque will be resisted by St. Venant tor-que and warping tortor-que, which can be regarded as semi- and quasi-tangential torques, respectively. However, the ratio of St. Venant torque to warping torque is not known before the torsional equation is solved [5].
0045-7825/$ - see front matter Ó 2007 Elsevier B.V. All rights reserved. doi:10.1016/j.cma.2007.07.028
DOI of original article:10.1016/j.cma.2006.07.013
*
Corresponding author.
E-mail address:ybyang@ntu.edu.tw(Y.B. Yang).
www.elsevier.com/locate/cma
Available online at www.sciencedirect.com
(6) Although some physical meanings were given for the terms containing the factor 1/2 in Eq. (15), they were there only for the interest of researchers familiar with the rotational properties of internal moments. (7) With regard to ‘‘external torques’’, i.e., those
gener-ated by mechanical devices, it is essential that the rotational increments generated by these devices upon three-dimensional rotations be duly taken into account in establishing the ‘‘joint equilibrium condi-tions’’ in the deformed state, as was stated in Section 5 of the paper, or in more details in Sections 6.3 and 6.7 of Yang and Kuo[4]. There is no argument that different ‘‘external moments’’ will result in different buckling loads. In fact, the same problem as the one presented by the discusser was analyzed by Yang and Kuo[3]via consideration of ‘‘element’’ equations and ‘joint’’ equations in the deformed state, in which distinction has been made between the ‘‘internal’’ and ‘‘external’’ moments with no consideration made for the factor 1/2 or a.
The authors would like to thank the discusser for bring-ing this issue here. We wish that the explanations given above can help clarify the problem.
References
[1] J.H. Argyris, O. Hilbert, G.A. Malejannakis, D.W. Scharpf, On the geometrical stiffness of a beam in space – a consistent v.w. approach, Comp. Methods Appl. Mech. Engrg. 20 (1979) 105– 131.
[2] Z.M. Elias, Theory and Methods of Structural Analysis, John Wiley, New York, NY, 1986.
[3] Y.B. Yang, S.R. Kuo, Buckling of frames under various torsional loadings, J. Engrg. Mech. ASCE 117 (8) (1991) 1681– 1697.
[4] Y.B. Yang, S.R. Kuo, Theory and Analysis of Nonlinear Framed Structures, Prentice-Hall, Englewood Cliffs, NJ, 1994.
[5] Y.B. Yang, W. McGuire, A procedure for analyzing space frames with partial warping restraint, Int. J. Numer. Meth. Engrg. 20 (1984) 1377– 1389.
[6] Y.B. Yang, W. McGuire, Stiffness matrix for geometric nonlinear analysis, J. Struct. Engrg., ASCE 112 (4) (1986) 853–877.