 
          3397
        
        
          Technical Committee 307 + 212 /
        
        
          
            Comité technique 307 + 212
          
        
        
          where
        
        
          
        
        
          and
        
        
          
        
        
          are the normal and shear stress acting on a fiber
        
        
          of a cross section of the micropile and
        
        
          
        
        
          e
        
        
          is the tensile strength
        
        
          of the steel.
        
        
          
        
        
          and
        
        
          
        
        
          will be expressed in terms of the normal
        
        
          force (
        
        
          
            N
          
        
        
          ), shear force (
        
        
          
            Q
          
        
        
          ) and bending moment (
        
        
          
            M
          
        
        
          ).
        
        
          The conditions leading to the maximum support provided by
        
        
          the micropile will be defined by those leading to the yielding of
        
        
          the most stressed fiber within the critically loaded steel cross
        
        
          section of the micropile. This section is point P in Figure 1.
        
        
          Forces
        
        
          
            N
          
        
        
          and
        
        
          
            Q
          
        
        
          and moment
        
        
          
            M
          
        
        
          at point P, due to an imposed
        
        
          displacement
        
        
          
        
        
          can be calculated if the mechanical and
        
        
          geometrical parameters of the micropile are known:
        
        
          2
        
        
          6
        
        
          
            x
          
        
        
          
            v
          
        
        
          
            EI
          
        
        
          
            M
          
        
        
          
            b
          
        
        
           
        
        
          ;
        
        
          3
        
        
          12
        
        
          
            x
          
        
        
          
            v
          
        
        
          
            EI
          
        
        
          
            Q
          
        
        
          
            b
          
        
        
          
        
        
          
        
        
          ;
        
        
          
            h
          
        
        
          
            AE N
          
        
        
          
            b
          
        
        
           
        
        
          (5a;b;c)
        
        
          where
        
        
          
            E
          
        
        
          is the steel elastic modulus,
        
        
          
            I
          
        
        
          
            x
          
        
        
          is the moment of inertia
        
        
          with respect to the horizontal axis of the section and
        
        
          
            A
          
        
        
          is the
        
        
          cross-sectional area of the micropile (a steel tubular section has
        
        
          been choosen having a diameter
        
        
          
            d
          
        
        
          and thickness
        
        
          
            t
          
        
        
          ).
        
        
          
        
        
          
            h
          
        
        
          =
        
        
          
        
        
          cos
        
        
          
        
        
          and
        
        
          
        
        
          
            v
          
        
        
          =
        
        
          
        
        
          cos
        
        
          
        
        
          are the horizontal and vertical components of the
        
        
          imposed displacement,
        
        
          
        
        
          expressed in terms of the angle
        
        
          
        
        
          (Eq.(2)).
        
        
          Under these conditions, normal and shear stresses due to the
        
        
          normal (
        
        
          
            N
          
        
        
          ) and shear (
        
        
          
            Q
          
        
        
          ) forces and moment (
        
        
          
            M
          
        
        
          ) are calculated:
        
        
          
            x
          
        
        
          
            N M z
          
        
        
          
            A I
          
        
        
          
        
        
           
        
        
          (6a)
        
        
          2
        
        
          2
        
        
          2
        
        
          2
        
        
          4
        
        
          2
        
        
          
            x
          
        
        
          
            x
          
        
        
          
            QS Q d z
          
        
        
          
            I t
          
        
        
          
            d t
          
        
        
          
        
        
            
        
        
          
        
        
          
        
        
          (6b)
        
        
          where z is the distance from the beam axis (
        
        
          
            x
          
        
        
          direction) to a
        
        
          particular point of the section and
        
        
          
            S
          
        
        
          
            x
          
        
        
          is the static moment of the
        
        
          cross-sectional area above coordinate
        
        
          
            z
          
        
        
          .
        
        
          Substituting
        
        
          
            N
          
        
        
          ,
        
        
          
            Q
          
        
        
          and
        
        
          
            M
          
        
        
          from Equations (5) into Equations
        
        
          (6) and the resulting expressions for
        
        
          
        
        
          and
        
        
          
        
        
          into Equation (4),
        
        
          the Von Mises criterion can be written.
        
        
          (a)
        
        
          (b)
        
        
          (c)
        
        
          Figure 3. (a) Isolated micropile subjected to an imposed displacement
        
        
          
        
        
          ;
        
        
          (b) bending behavior of the micropile; (c) tensile behavior of the
        
        
          micropile.
        
        
          A conservative assumption is now introduced in the
        
        
          calculation. The available strength provided by the micropile is
        
        
          calculated as the value associated with the state in which the
        
        
          section starts to yield at some fiber. Therefore, the stress
        
        
          provided by the micropile beyond this point, due to the yielding
        
        
          of the rest of the section, is not considered here.
        
        
          The shear stress
        
        
          
        
        
          reaches a maximum in the center of the
        
        
          section. On contrary, the stress
        
        
          
        
        
          due to
        
        
          
            N
          
        
        
          and
        
        
          
            M
          
        
        
          reaches a
        
        
          maximum at
        
        
          
            z
          
        
        
          = -
        
        
          
            R
          
        
        
          
        
        
          Bending dominates the tensile stressing of
        
        
          the micropile for the particular problem we are considering due
        
        
          to the particular cross-section of the micropiles and the imposed
        
        
          loading mechanism.
        
        
          
        
        
          t turns out that the critical stress is located
        
        
          at the outer part of the cross section.
        
        
          Applying Von Mises’ criterion (Eq. 4) to the fiber
        
        
          characterized by z = -
        
        
          
            R
          
        
        
          the following expression for the
        
        
          displacement,
        
        
          
        
        
          , leading to the first fiber yielding in the
        
        
          micropile cross section at point P is derived:
        
        
          
        
        
          
        
        
          1
        
        
          ,
        
        
          
            t
          
        
        
          
            b
          
        
        
          
            E f d b
          
        
        
          
        
        
           
        
        
          
        
        
          (7)
        
        
          where
        
        
          
            f
          
        
        
          (
        
        
          
            d
          
        
        
          /
        
        
          
            b
          
        
        
          ,
        
        
          
        
        
          ) is a function of the ratio between the diameter of
        
        
          the micropile (
        
        
          
            d
          
        
        
          ) and the equivalent length of the beam (
        
        
          
            b
          
        
        
          ) and
        
        
          the relative orientation between the micropile and the upper
        
        
          sliding wedge of the failure mechanism (
        
        
          
        
        
          ) (Eq. (2)):
        
        
          
        
        
          
        
        
           
        
        
           
        
        
          2
        
        
          2
        
        
          2
        
        
          ,
        
        
          6 cos sin
        
        
          9 sin
        
        
          cos
        
        
          
            f d b
          
        
        
          
            d b
          
        
        
          
            d b
          
        
        
               
        
        
           
        
        
          (8)
        
        
          Finally, when the value of
        
        
          
        
        
          given in Equation (7) is
        
        
          substituted into equation (5b and c), the following shear and
        
        
          tensile forces applied by the micropile on the sliding
        
        
          mechanism, at point P, are found:
        
        
          
        
        
          
        
        
          cos
        
        
          ,
        
        
          
            e
          
        
        
          
            N td
          
        
        
          
            f d b
          
        
        
          
        
        
            
        
        
          
        
        
          (9a)
        
        
           
        
        
          
        
        
          
        
        
          2
        
        
          3
        
        
          c
        
        
          2
        
        
          ,
        
        
          
            e
          
        
        
          
            Q td d b
          
        
        
          
            f d b
          
        
        
          os
        
        
          
        
        
            
        
        
          
        
        
          (9b)
        
        
          These expressions for
        
        
          
            N
          
        
        
          and
        
        
          
            Q
          
        
        
          are now introduced into Eq.
        
        
          (1) to find the external loads that leads to the defined failure
        
        
          mechanism. The resulting equation is:
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
           
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          2
        
        
          4
        
        
          1
        
        
          3
        
        
          5
        
        
          1
        
        
          2
        
        
          3
        
        
          4
        
        
          5
        
        
          1
        
        
          2
        
        
          3
        
        
          4
        
        
          5
        
        
          1
        
        
          2
        
        
          3
        
        
          4
        
        
          5
        
        
          1
        
        
          2
        
        
          3
        
        
          4
        
        
          5
        
        
          2
        
        
          2
        
        
          2
        
        
          2
        
        
          4
        
        
          1
        
        
          3
        
        
          5
        
        
          sin sin
        
        
          2
        
        
          sin sin sin cos
        
        
          1
        
        
          2
        
        
          2
        
        
          2
        
        
          1
        
        
          tan tan tan tan tan
        
        
          cos
        
        
          1
        
        
          sin cos
        
        
          2
        
        
          cos 1.5sin
        
        
          sin sin
        
        
          sin sin sin
        
        
          ,
        
        
          
            s
          
        
        
          
            T
          
        
        
          
            u
          
        
        
          
            u
          
        
        
          
            e
          
        
        
          
            u
          
        
        
          
            C
          
        
        
          
            c
          
        
        
          
            D
          
        
        
          
            D C
          
        
        
          
            c D
          
        
        
          
            d b
          
        
        
          
            td
          
        
        
          
            Dc s
          
        
        
          
            f d b
          
        
        
            
        
        
           
        
        
          
        
        
          
        
        
                     
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
                
        
        
           
        
        
          
        
        
          
        
        
           
        
        
          
        
        
          
        
        
                   
        
        
          
        
        
          
        
        
            
        
        
          
        
        
          
        
        
           
        
        
           
        
        
            
        
        
          
        
        
          0
        
        
          (10)
        
        
          Notice that the fist term identifies the external forces
        
        
          without including the micropile. This term will be referred to as
        
        
          the “External Stress Coefficient”. The reinforcement is
        
        
          identified by the dimensionless parameter
        
        
          
            e
          
        
        
          
            td Dc s
          
        
        
          
        
        
          
            u
          
        
        
          which
        
        
          combines in a simple expression the mechanical properties of
        
        
          the tubular reinforcement (
        
        
          
        
        
          
            e
          
        
        
          ,
        
        
          
            t
          
        
        
          and
        
        
          
            d
          
        
        
          ), the undrained soil
        
        
          strength (
        
        
          
            c
          
        
        
          
            u
          
        
        
          ) and the spacing between micropiles axis (
        
        
          
            s
          
        
        
          ). This
        
        
          ratio will be named the “Micropile Coefficient”.
        
        
          The most critical collapse mechanisms will be calculated
        
        
          optimizing the energy conservation equation with respect to the
        
        
          five angles describing the geometry.
        
        
          
            2.4 Upper bound solution for the External Stress
          
        
        
          
            Coefficient
          
        
        
          The coefficient (
        
        
          
        
        
          s
        
        
          -
        
        
          
        
        
          
        
        
          )/c
        
        
          u
        
        
          has been isolated from Equation (10)
        
        
          and minimized with respect to the angles in order to find the
        
        
          smallest upper bound solution linked to the mechanism
        
        
          proposed. The upper bound solution obtained depends on
        
        
          
        
        
          
            D/c
          
        
        
          
            u
          
        
        
          ,
        
        
          on the Micropile Coefficient and on the cover ratio
        
        
          
            C/D.
          
        
        
          The set of parameters defining the problem have been
        
        
          collected in Table 1. The table indicates also the range of values
        
        
          typically encountered in practice. Three values of the Micropile
        
        
          Coefficient (0, 20 and 50) have been selected to plot the
        
        
          minimized values of the External Stress Coefficient (with
        
        
          respect to the five angles) against the cover ratio
        
        
          
            C/D
          
        
        
          for
        
        
          different values of the strength ratio
        
        
          
        
        
          
            D/c
          
        
        
          
            u
          
        
        
          (Fig. 4). The adopted
        
        
          values of
        
        
          
            b,
          
        
        
          that defines the clamped length of the micropiles
        
        
          (Fig. 2), is five times the micropiles diameter (
        
        
          
            d
          
        
        
          ).