Skip to main content

Table 2 Chord deformations of VATM by the principles of virtual work method.

From: Theoretical and Experimental Study of Effective Shear Stiffness of Reinforced ECC Columns

Member

Force

Unit load

Length

Rigidity

Deformation

F

f

l

EA

Ffl/EA

BD

\( - \frac{{dV_{t} }}{{\sin \theta_{1} }} \)

\( - \frac{1}{{\sin \theta_{1} }} \)

\( \frac{{d_{v} }}{{\sin \theta_{1} }} \)

\( \frac{{E_{c} bL\sin \theta_{1} dx}}{2} \)

\( \frac{{2d_{v} dV_{t} }}{{E_{c} bL\sin^{4} \theta_{1} dx}} \)

CE

\( - \frac{{dV_{t} }}{{\sin \theta_{2} }} \)

\( - \frac{1}{{\sin \theta_{2} }} \)

\( \frac{{d_{v} }}{{\sin \theta_{2} }} \)

\( \frac{{E_{c} bL\sin \theta_{2} dx}}{2} \)

\( \frac{{2d_{v} dV_{t} }}{{E_{c} bL\sin^{4} \theta_{2} dx}} \)

BE

+ dV t

+ 1

d v

\( E_{s} \left( {\frac{{A_{sh} }}{s} + \frac{b}{n}} \right)Ldx \)

\( \frac{{d_{v} dV_{t} }}{{E_{s} \left( {\frac{{A_{sh} }}{s} + \frac{b}{n}} \right)Ldx}} \)