 
          2693
        
        
          Technical Committee 212 /
        
        
          
            Comité technique 212
          
        
        
          coefficients (
        
        
          α
        
        
          ) and (
        
        
          β
        
        
          ) was used to define in each layer and the
        
        
          coefficients were determined from the relationship given below:
        
        
          i i
        
        
          i
        
        
          D
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          2
        
        
          2
        
        
           
        
        
          (1)
        
        
          where
        
        
          D
        
        
          i
        
        
          = damping ratio corresponding to frequency of
        
        
          vibration
        
        
          ω
        
        
          i
        
        
          It was assumed that 60 rad/sec and 500 rad/sec were the limit
        
        
          of predominant frequencies in dynamic testing i.e., all damping
        
        
          values for different layers were less than the damping values
        
        
          (
        
        
          D
        
        
          1
        
        
          ,
        
        
          D
        
        
          2
        
        
          ) considered here in this frequency range. The damping
        
        
          values were taken from guidelines given by Bowles (1996).
        
        
          Finally the (
        
        
          α
        
        
          ) and (
        
        
          β
        
        
          ) coefficients were calculated by using Eq.
        
        
          (1).
        
        
          The model was analysed in three calculation phases. First
        
        
          gravity analysis was performed only in soil mass in vertical
        
        
          Z
        
        
          direction. In the next step, the pile-soil interaction was
        
        
          introduced as well as static load was applied on the top of the
        
        
          pile. A steel plate was provided on the pile head to simulate the
        
        
          exact static load (8 kN and 10 kN) applied on pile. In the third
        
        
          phase the dynamic FE analysis was performed by applying
        
        
          sinusoidal vertical load on the pile using a dynamic multiplier
        
        
          function at wide range of frequencies (5 to 60 Hz). According to
        
        
          the values of eccentric moments (0.278 Nm, 0.366 Nm, 0.450
        
        
          Nm and 0.529 Nm) and operating frequency of the motor, the
        
        
          dynamic load amplitudes were determined.
        
        
          4 RESULTS AND DISCUSSION
        
        
          4.1 Validation of finite-element model
        
        
          To monitor the boundary effect, the model was analysed with
        
        
          different radius of boundaries. Based on the results, the
        
        
          boundaries of soil mass around the pile were considered with a
        
        
          radius of 30 m and height of 45 m to avoid the direct influence
        
        
          of the boundary conditions. Static load analysis was carried out
        
        
          and the results obtained from FE analysis were compared with
        
        
          the static load test results. The comparison of static load test
        
        
          results with the FE analysis is shown in Figure. 3. The predicted
        
        
          settlement obtained from FE analysis is approximately 1.45 mm
        
        
          and observed settlement is 1.45 mm and 2.3 mm for pile 1 and
        
        
          pile 2 respectively at calculated safe load (283 kN).
        
        
          Figure 3. Comparison of load verses settlement curve obtained from FE
        
        
          analysis and static load test.
        
        
          4.2 Comparison between finite-element analysis and dynamic
        
        
          test results
        
        
          The time versus amplitude curves were obtained from FE
        
        
          analysis at different operating frequencies of machine for
        
        
          different static load and eccentric moments. A typical response
        
        
          curve is presented in Figure. 4 for static load of 10 kN. From the
        
        
          time versus amplitude curves, the frequency versus amplitude
        
        
          curves were obtained and compared with the field vibration test
        
        
          results.
        
        
          Figure 4. Time-amplitude response of pile at different frequencies (FE
        
        
          analysis).
        
        
          The typical comparison of frequency-amplitude response
        
        
          obtained from FE analysis and test results are shown in Figure.
        
        
          5 and Figure 6 for pile 1 and pile 2 respectively.
        
        
          Figure 5. Comparison of frequency-amplitude curve obtained from FE
        
        
          analysis and dynamic test results (Pile 1).
        
        
          It is found from these figures that the predicted resonant
        
        
          frequency and amplitude are very close to the vertical vibration
        
        
          test results. The resonant frequencies are decreased with the
        
        
          increase of eccentric moments under same static load. This
        
        
          phenomenon indicates the nonlinear behaviour of soil-pile
        
        
          system obtained from FE analysis which is similar to the field
        
        
          test results. This nonlinear response of the soil-pile system is
        
        
          due to the material nonlinearity which is nothing but reduction