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Mechanics-based modal identification of thin-walled members with multi-branched cross-sections by: S. Ádány and B.W. Schafer. McMat 2005 2005 Joint ASME/ASCE/SES Conference on Mechanics and Materials Baton Rouge, Louisiana June 2, 2005. motivation
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Mechanics-based modal identification of thin-walled members with multi-branched cross-sections by: S. Ádány and B.W. Schafer McMat 2005 2005 Joint ASME/ASCE/SES Conference on Mechanics and Materials Baton Rouge, Louisiana June 2, 2005
motivation • mechanical criteria for modal decomposition / identification • framework for FSM implementation • brief example • details of FSM implementation including multi-branched sections • concluding thoughts
local buckling distortional buckling lateral-torsional buckling stability mode identification in a thin-walled member FSM Mcr Lcr l FEM
GBT and modal identification (as Dinar has described!) • Advantages • modes look “right” • can focus on individual modes or subsets of modes • can identify modes within a more general GBT analysis • Disadvantages • development is unconventional/non-trivial, results in the mechanics being partially obscured (opinion) • not widely available for use in programs • Extension to general purpose FE awkward • We identified the key mechanical assumptions of GBT and then implemented them in FSM (FEM) to enable these methods to perform GBT-like “modal” solutions.
criteria: #1 membrane restriction #2 non-zero warping #3 no transverse bending mechanical assumptions of GBT modes #1 #2 #3
FSM modal decomposition (identification) • Begin with our standard stability (eigen) problem • Now introduce a set of constraints consistent with a desired modal definition, this is embodied in R • Pre-multiply by RT and we create a new, reduced stability problem that is in a space with restricted degree of freedom, if we choose R appropriately we can reduce down to as little as one “modal” DOF
brief example... implemented in open source matlab-based finite strip software www.ce.jhu.edu/bschafer
#1 #2 #3 FSM implementation details... u,v: membrane plane stress w,q: thin plate bending
general displacement vector: d=[U V W Q]T constrained to distortional: d=Rdr, dr=[V] • u(i)-v1,2 relation via membrane assumptions (#1) • u(i-1,i)-Vi-1,i,i+1 relation considering connectivity • u(i-1,i),w(i-1,i)-Ui,Wi by coord. transformation subset of this: u(i-1,i)-Ui,Wi relation • Ui,Wi-Vi-1,i,i+1 through combining above • Qi-Ui,Wi relation through beam analogy (#3) notations: superscript= elements, subscript = nodes, lowercase = local, uppercase = global
u(i)-v1,2 relation FSM shape functions membrane restriction: resulting relation:
u(i-1),(i)-Vi-1,i,i+1 relation element (i-1): element (i): connectivity:
u(i-1),(i)-UiWi relation local-global transform: element (i-1): element (i):
UiWi-Vi-1,i,i+1 relation local-global transform membrane assumption + connectivity
multi-branched: u(i)-v1,2 relation membrane restriction results in:
multi-branched: u(i-1),(i)-UiWi relation (cont.) single-branched: multi-branched: The multi-branched case is over-determined (heart of the issue for a multi-branched section):
multi-branched: UiWi-Vi-1,i,i+1 relation multi-branch case leads to additional constraints on V....
concluding thoughts • Current general purpose FSM (FEM) methods are uncapable of modal identification / decomposition for thin-walled member stability modes • Inspired by GBT, the modes (i.e., G, D, L, O classes of modes) are postulated as mechanical constraints • Modal definitions are implemented in an FSM context for singly and multi-branched sections • Formal modal definitions enable FSM to perform • Modal decomposition (focus on a given mode) • Modal identification (figure out what you have) • Much work remains, and definitions are not perfect
acknowledgments • Thomas Cholnoky Foundation • Hungarian Scientific Research Fund • U.S., National Science Foundation
Q-U,V relation U,W displacements reconciled through Q and beam analogy U,W are “support displacements”
Membrane (plane stress) FSM Ke = Kem + Keb
Thin plate bending FSM Ke = Kem + Keb
finite strip method • Capable of providing complete solution for all buckling modes of a thin-walled member • Elements follow simple mechanics bending • w, cubic “beam” shape function • thin plate theory membrane • u,v, linear shape functions • plane stress conditions • Drawbacks: special boundary conditions, no variation along the length, cannot decompose, nor help identify “mechanics-based” buckling modes
Experiments on cold-formed steel columns 267 columns , b = 2.5, f = 0.84