A Hertzian contact model is used here and so the normal (incremental) stiffness (\({k}_{N})\) depends on the diameters of the contacting particles and the contact force, as follows:
$${k}_{N}=2{E}_{p}^{*}{{R}^{*}}^{0.5}{\delta }^{0.5}$$
(9)
where \(\delta\) is the contact overlap and \({R}^{*}={(1/{R}_{1}+1/{R}_{2})}^{-1}\), \({R}_{1}\) and \({R}_{2}\) are the radii of the contacting particles. The equivalent Young’s modulus of the two contacting particles,\({E}_{p}^{*}\) is:
$${E}_{p}^{*}={\left(\frac{1-{v}_{p1}^{2}}{{E}_{p1}}+\frac{1-{v}_{p2}^{2}}{{E}_{p2}}\right)}^{-1}$$
(10)
where \({E}_{p1}\) and \({E}_{p2}\) are the Young’s moduli of the contacting particles, and \({v}_{p1}\) and \({v}_{p2}\) are the Poisson’s ratios of the contacting particles. The tangential or shear contact stiffness is:
$${k}_{T}=8{G}_{p}^{*}a$$
(11)
where \({G}_{p}^{*}\), the equivalent shear modulus of the two contacting particles is:
$${G}_{p}^{*}={\left(\frac{2-{v}_{p1}}{{G}_{p1}}+\frac{2-{v}_{p2}}{{G}_{p2}}\right)}^{-1}$$
(12)
and \({G}_{p1}\) and \({G}_{p2}\) are the shear moduli of the contacting particles and the radius of the circular contact are \(a=\sqrt{{R}^{*}\delta }\).
Figure 11a is a scatter plot of the normal stiffness, \({k}_{N}\), values versus the normal force value for each contact point for the dense linear specimens. In all cases, the contact normal stiffness increases with increasing normal force, however there is a wide range of stiffness values and there is no clear difference amongst the linear specimens considered here. Figure 11b shows the cumulative distribution of the normal stiffnesses, while Fig. 11c shows the data normalised by the mean normal stiffness respectively. While no significant differences can be identified amongst these specimens, the range of \({k}_{N}\) values increases with increasing \({C}_{u}\).
Figure 12a–c are scatter plots of the \({k}_{N}\) values versus the normal force for each contact point for representative bimodal gap-graded specimens with \(SR\) = 8.4, and with \({F}_{finer}\) of 10%, 25% and 50% respectively. There is a clear difference between the three different contact types in these specimens. For all three \({F}_{finer}\) values considered, the maximum contact force between two coarse particles (\(C-C\)) is significantly larger than the maximum contact force between a coarser and finer particle (\(C-F\)) which in turn is larger than the maximum contact force between two finer particles (\(F-F\)). Each contact type exhibits a different relationship between normal force and normal stiffness, so that, at a given normal force, the \(C-C\) contacts have the highest normal stiffness and the \(F-F\) contacts have the lowest contact stiffness. This heterogeneity reflects a complex interdependency of force and stiffness; \({k}_{n}\) depends upon on the effective radius. However, assuming that there is no generation and no loss of contacts when a small increment in uniform strain is applied, the increase in force at the stiffer contacts will be larger. Figure 12d presents the cumulative distribution, by number of contacts, of the normal stiffness for the dense bimodal specimens with \(SR\) of 8.4; a distinct behaviour can be observed between the underfilled specimens (i.e. \({F}_{finer}\) of 5%, 10%, 15% and 20%) and overfilled conditions (\({F}_{finer}\) of 25%, 30%, 35% and 50%). The significantly higher contact stiffness values when \({F}_{finer}<\) 20%, reflect the large stiffness values associated with the \(C-C\) contacts. At \({F}_{finer}=\) 20%, the cumulative distribution indicates a mix of small contact stiffnesses and large contact siffnesses. Then for \({F}_{finer}\ge\) 20%, there is a more continuous distribution showing normal stiffness, while these finer related contacts show relatively small normal stiffness values in the overfilled case. Figure 12e presents the results for the loose condition with similar trends being identified. These data highlight the fact that contacts between particles of differenct sizes have measurable differences in stiffness; this has not always been considered in attempts to develop frameworks to predict \({G}_{0}\).
Stiffness matrix approach to consider contributions of contacts to overall stiffness
While looking at the distribution of stiffness values amongst the contacts gives useful insight into the system, these values cannot be directly related to the overall shear stiffness and the orientation of the contacts relative to the overall deformation field is not considered. Contacts in a physical granular material form a relatively complex network and the properties of the network edges depend upon the contact orientations, the effective radii, and the transmitted contact forces. These characteristics cannot be directly captured considering only the contact stiffness values. To further advance our understanding we used a stiffness-matrix based approach to consider the contribution of each contact to the global stress field when a uniform strain field is assumed to describe the motion of all the particles. In this approach, following the procedure outlined in Itasca Consulting Group [9], a local stiffness matrix \({k}^{ab}\) is defined for the contact between particles \(a\) and \(b\). For clarity, a representative 12 \(\times\) 12 element stiffness matrix in the case where the contact normal is orientated along the \(x-\) axis is given here as:
$${k}^{ab,nx}=\left[\begin{array}{ccc}\begin{array}{ccc}{K}_{N}& & \\ 0& {K}_{T}& \\ 0& 0& {K}_{T}\end{array}& \begin{array}{ccc} & & \\ & & \\ & & \end{array}& \begin{array}{ccc}& & \begin{array}{ccc}& & \begin{array}{cc}& \end{array}\end{array}\\ & & \begin{array}{ccc}& & \begin{array}{cc}& \end{array}\end{array}\\ & & \begin{array}{ccc}& & \begin{array}{cc}& \end{array}\end{array}\end{array}\\ \begin{array}{ccc}0& 0& 0\\ 0& 0& {-{R}^{*}K}_{T}\\ 0& {{R}^{*}K}_{T}& 0\end{array}& \begin{array}{ccc}0& & symmetry\\ 0& {{{R}^{*}}^{2}K}_{T}& \\ 0& 0& {{{R}^{*}}^{2}K}_{T}\end{array}& \begin{array}{ccc}& & \begin{array}{ccc}& & \begin{array}{cc}& \end{array}\end{array}\\ & & \begin{array}{ccc}& & \begin{array}{cc}& \end{array}\end{array}\\ & & \begin{array}{ccc}& & \begin{array}{cc}& \end{array}\end{array}\end{array}\\ \begin{array}{ccc}{-K}_{N}& 0& 0\\ 0& -{K}_{T}& 0\\ \begin{array}{c}0\\ 0\\ \begin{array}{c}0\\ 0\end{array}\end{array}& \begin{array}{c}0\\ 0\\ \begin{array}{c}0\\ {{R}^{*}K}_{T}\end{array}\end{array}& \begin{array}{c}-{K}_{T}\\ 0\\ \begin{array}{c}{{R}^{*}K}_{T}\\ 0\end{array}\end{array}\end{array}& \begin{array}{ccc}0& 0& 0\\ 0& 0& {-{R}^{*}K}_{T}\\ \begin{array}{c}0\\ 0\\ \begin{array}{c}0\\ 0\end{array}\end{array}& \begin{array}{c}{{R}^{*}K}_{T}\\ 0\\ \begin{array}{c}{{{R}^{*}}^{2}K}_{T}\\ 0\end{array}\end{array}& \begin{array}{c}0\\ 0\\ \begin{array}{c}0\\ {{{R}^{*}}^{2}K}_{T}\end{array}\end{array}\end{array}& \begin{array}{ccc}{K}_{N}& & \begin{array}{ccc}& & \begin{array}{cc}& \end{array}\end{array}\\ 0& {K}_{T}& \begin{array}{ccc}& & \begin{array}{cc}& \end{array}\end{array}\\ \begin{array}{c}0\\ 0\\ \begin{array}{c}0\\ 0\end{array}\end{array}& \begin{array}{c}0\\ 0\\ \begin{array}{c}0\\ {-{R}^{*}K}_{T}\end{array}\end{array}& \begin{array}{c}\begin{array}{ccc}{K}_{T}& & \begin{array}{cc}& \end{array}\end{array}\\ \begin{array}{ccc}0& 0& \begin{array}{cc}& \end{array}\end{array}\\ \begin{array}{c}\begin{array}{ccc}{{R}^{*}K}_{T}& 0& \begin{array}{cc}{{{R}^{*}}^{2}K}_{T}& \end{array}\end{array}\\ \begin{array}{ccc}0& 0& \begin{array}{cc}0& {{{R}^{*}}^{2}K}_{T}\end{array}\end{array}\end{array}\end{array}\end{array}\end{array}\right]$$
(13)
The increment in the contact force vector induced by an increment in displacement of the two grains is given by:
$${{\varvec{\Delta}}{\varvec{f}}}^{ab}={k}^{ab}{{\varvec{\Delta}}{\varvec{x}}}^{ab}$$
(14)
where the incremental displacements of the two contacting particles are given by \({{\varvec{\Delta}}{\varvec{x}}}^{ab}=\left[\begin{array}{ccc}{\Delta x}_{1}^{a}& {\Delta x}_{2}^{a}& {\Delta x}_{3}^{a}\end{array}\Delta \begin{array}{ccc}{\theta }_{1}^{a}&\Delta {\theta }_{2}^{a}&\Delta {\theta }_{3}^{a}\end{array} \begin{array}{ccc}{\Delta x}_{1}^{b}& {\Delta x}_{2}^{b}& {\Delta x}_{3}^{b}\end{array}\Delta \begin{array}{ccc}{\theta }_{1}^{b}&\Delta {\theta }_{2}^{b}&\Delta {\theta }_{3}^{b}\end{array}\right]\), and the vector \({{\varvec{\Delta}}{\varvec{f}}}^{ab}\) gives both the increments in forces and moments at the interaction between particles \(a\) and \(b\).
Referring to Thornton [37], in a periodic cell, if the strain rate tensor applied to the periodic cell is given by \({\dot{\varepsilon }}_{ij}\), then in a timestep \(\Delta t\) the incremental displacement of particle \(a\) due to the global strain field, \({\Delta x}_{i}^{a}\) is \({\Delta x}_{i}^{a}={\dot{\varepsilon }}_{ij}{x}_{i}^{a}\Delta t\), where \({x}_{i}^{a}\) is the vector describing the location of particle \(a\). In a similar manner, if an increment of strain \({\Delta \varepsilon }_{ij}\) is applied to the system, the incremental displacement is given by:
$${\Delta x}_{i}^{a}={\Delta \varepsilon }_{ij}{x}_{i}^{a}$$
(15)
For simplicity, supposing that a deformation is small and assuming that the increment of branch vector \(\Delta {l}_{j}\approx 0\), \(\Delta V\approx 0\), and there are no newly generated contacts. If each contact experiences an incremental force, \(\Delta {f}_{i}^{c}\), then the resulting increment in stress is given by:
$${\Delta \sigma }_{ij}=\frac{1}{V}\sum_{c=1}^{{N}_{c}}{\Delta f}_{i}^{c}{l}_{j}^{c}$$
(16)
In engineering or Voigt notation the elasticity tensor \({D}_{ij}\) is given by:
$$\left[\begin{array}{c}\begin{array}{c}{\Delta \sigma }_{11}\\ {\Delta \sigma }_{22}\end{array}\\ \begin{array}{c}{\Delta \sigma }_{33}\\ {\Delta \sigma }_{23}\end{array}\\ \begin{array}{c}{\Delta \sigma }_{31}\\ {\Delta \sigma }_{12}\end{array}\end{array}\right]=\left[\begin{array}{ccc}\begin{array}{cc}{D}_{11}& {D}_{12}\\ & {D}_{22}\end{array}& \begin{array}{cc}{D}_{13}& {D}_{14}\\ {D}_{23}& {D}_{24}\end{array}& \begin{array}{cc}{D}_{15}& {D}_{16}\\ {D}_{25}& {D}_{26}\end{array}\\ \begin{array}{cc} & \\ & \end{array}& \begin{array}{cc}{D}_{33}& {D}_{34}\\ & {D}_{44}\end{array}& \begin{array}{cc}{D}_{35}& {D}_{36}\\ {D}_{45}& {D}_{46}\end{array}\\ \begin{array}{cc} & \\ & \end{array}& \begin{array}{cc} & \\ & \end{array}& \begin{array}{cc}{D}_{55}& {D}_{56}\\ & {D}_{66}\end{array}\end{array}\right]\left[\begin{array}{c}\begin{array}{c}{\Delta \varepsilon }_{11}\\ {\Delta \varepsilon }_{22}\end{array}\\ \begin{array}{c}{\Delta \varepsilon }_{33}\\ {2\Delta \varepsilon }_{23}\end{array}\\ \begin{array}{c}{2\Delta \varepsilon }_{13}\\ {2\Delta \varepsilon }_{12}\end{array}\end{array}\right]$$
(17)
This is a symmetric tensor and only the upper right-hand side of the tensor is given here. Here the stiffness matrices for each contact were determined from the data generated in the \(DEM\) simulations. The particle displacements due a specified \({\Delta \varepsilon }_{ij}\) were determined from Eq. (15) and the increment in force for each contact was determined using Eq. (14) before applying Eq. (17) to determine the increment in stress and hence elements of the stiffness matrix.
Based on the uniform strain approach assumption, the relative contributions of the different contact types to the stiffness can be estimated. Firstly, the overall stiffness \({D}_{ij}^{all}\) is estimated, then the contribution of each of the networks can be isolated: \(CC\) contribution: \(\frac{{D}_{ij}^{CC}}{{D}_{ij}^{all}}\); \(CF\) contribution: \(\frac{{D}_{ij}^{CF}}{{D}_{ij}^{all}}\); \(FF\) contribution: \(\frac{{D}_{ij}^{FF}}{{D}_{ij}^{all}}\).
Based up on the Love-Weber formula:
$${\sigma }_{ij}^{all}=\frac{1}{V}{\sum }_{c=1}^{{N}_{c}}{f}_{i}{l}_{j}=\frac{1}{V}\left({\sum }_{{c}^{CC}=1}^{{N}_{c}^{CC}}{f}_{i}{l}_{j}+{\sum }_{{c}^{CF}=1}^{{N}_{c}^{CF}}{f}_{i}{l}_{j}+{\sum }_{{c}^{FF}=1}^{{N}_{c}^{FF}}{f}_{i}{l}_{j}\right)$$
(18)
For simplicity, supposing that a deformation is small and assuming that \(\Delta {l}_{j}\approx 0\), \(\Delta V\approx 0\), and no newly generated contacts:
$$\Delta {\sigma }_{ij}^{all}=\frac{1}{V}\left(\sum _{{c}^{CC}=1}^{{N}_{c}^{CC}}\Delta {f}_{i}{l}_{j}+\sum _{{c}^{CF}=1}^{{N}_{c}^{CF}}\Delta {f}_{i}{l}_{j}+\sum _{{c}^{FF}=1}^{{N}_{c}^{FF}}\Delta {f}_{i}{l}_{j}\right)$$
(19)
For example, a strain field \(\Delta {\upvarepsilon }_{\mathrm{ij}}>0,\Delta {\upvarepsilon }_{\mathrm{other}}=0\) is imposed to the system.
$${D}_{ij}^{all}=\frac{\Delta {\sigma }_{ij}^{all}}{\Delta {\varepsilon }_{ij}}$$
(20)
In this case, based on elastic theory, \({G}_{0}\) can be calculated as \(0.25\times ({D}_{13}+{D}_{31})\), where \({D}_{13}\) and \({D}_{31}\) are defined in Eq. (17). This stiffness matrix method therefore estimates the \({G}_{0}\) over the whole specimen. And the stiffness contribution of each fraction (i.e. coarse and finer fraction) can also be estimated. Figure 13 compares the stiffness values from the probe and the matrix method. For the dense specimens, as shown in Fig. 13a, the probe and the matrix methods give similar trends when the variation in \({G}_{0}\) with \({C}_{u}\) is considered. However, the stiffness values obtained from the matrix method consistently exceed those obtained from the probe method. This may be attributed to the uniform strain assumption underlying the stiffness matrix approach. Yimsiri & Soga [43] and Magnanimo et al. [17] amongst others have highlighted the inability of \(EMT\) to accurately capture the variation in stiffness amongst soil specimens. The limitations of this kinematic assumption [12, 13, 18] likely explain the overestimation of the stiffness values. However, upon normalization, the matrix approach predicts the same state-dependency stiffness as observed in the data acquired using the probe method. Referring to Fig. 13b, if the \({G}_{0}\) data obtained at 500 \(kPa\) are normalized by the data at 100 \(kPa\), the responses are equivalent for both probe and matrix methods.
Figure 14a shows the variation in the \({G}_{0}\) values from both probe and matrix methods for the bimodal specimens with \(SR\) = 8.4. As in the case of the linear specimens \({G}_{0}^{matrix}\) values are consistently larger than the \({G}_{0}\) data obtained using the probe method. However, \({G}_{0}\) and \({G}_{0}^{matrix}\) values exhibit similar trends. This is confirmed in Fig. 14b. Figure 14b shows that at a given\({F}_{finer}\), the \({G}_{0}\) values at 500 \(kPa\) normalized by the \({G}_{0}\) values at 100\(kPa\), i.e. \({G}_{0}^{500 kPa}/{G}_{0}^{100 kPa}\), obtained using both methods are very similar. Both approaches predict very similar trends. Overall, while this matrix method overestimates\({G}_{0}\), it can capture the variation in \({G}_{0}\) with state and the key factors that contribute to this overall stiffness.
Heterogeneity of stress amongst particles
To link the stiffness distribution to the particle-scale stress distribution, two approaches were used to quantify the distribution of stress amongst the different particle sizes in these specimens. In the first, particle-based approach, the overall stress tensor can be determined from the stress tensors for the individual particles as:
$$\sigma_{ij}^{\prime } = \frac{1}{V}\mathop \sum \limits_{a = 1}^{{N_{t} }} \left( {\overline{\sigma }_{ij}^{a} V^{a} } \right)$$
(21)
where \(\sigma_{ij}^{\prime }\) is the effective overall stress tensor for the specimen, \({N}_{t}\) is the total number of stress-transmitting particles, \({\overline{\sigma }}_{ij}^{a}\) is the average stress tensor within particle \(a\), and \({V}^{a}\) is the volume of particle \(a\) (e.g. [29]. The contribution of an individual particle, \(a\), to the overall stress, \({\widehat{\sigma }}_{ij}^{a}\) is then given by:
$${\widehat{\sigma }}_{ij}^{a}=\frac{{\overline{\sigma }}_{ij}^{a} {V}^{a}}{V}$$
(22)
In the second, contact-based approach, the contact force data were used to calculate the stresses in the virtual specimen so that the \(3D\) stress tensor is given by:
$$\sigma_{ij}^{\prime } = \frac{1}{V}\mathop \sum \limits_{c = 1}^{{N_{c,V} }} {\varvec{f}}_{i}^{c} {\varvec{l}}_{j}^{c}$$
(23)
where \({N}_{c,V}\) is the total number of contacts in volume \(V\), \({{\varvec{f}}}_{i}^{c}\) is the force vector for contact \(c\) and \({{\varvec{l}}}_{j}^{c}\) is the branch vector, i.e. the vector joining the centroids of the particles which contact at \(c\) (e.g. [1]. The contribution of contact \(c\) to the overall stress,\({\widehat{\sigma }}_{ij}^{c}\) is:
$${\widehat{\sigma }}_{ij}^{c}=\frac{{{\varvec{f}}}_{i}^{c}{{\varvec{l}}}_{j}^{c}}{V}$$
(24)
Figure 15a shows the PSDs for all the linear specimens considered, where the particle diameter is normalized by the maximum particle size, i.e. \({d}^{p}\)/\({d}_{M}^{p}\). By adopting Eq. (22), the cumulative distribution of each particle to the macro-scale mean effective stress (\(\sigma_{ij}^{\prime }\)) is presented in Fig. 15b, defined as PSDstress. By adopting Eq. (23), the cumulative distribution of the contribution of each contact to macro-scale mean effective stress (\(\sigma_{ij}^{\prime }\)), \({CSD}^{stress}\) is presented in Fig. 15c. The x– axis is the branch vector length normalised by the maximum branch vector identified for the relevant simulation, \(\left| {l^{c} } \right|/\left| {l_{M}^{pc} } \right|\).
In the stiffness matrix approach, the overall stiffness is determined from a summation over all of the contacts, and so the contribution of each of contact can be isolated. These data can be used to plot the cumulative distribution of the contribution of contacts with different branch vector lengths to the overall stiffness, \({CSD}^{stiffness}\). By adopting Eq. (20), the cumulative distribution of the contribution of each contact to the overall stiffness is presented in Fig. 15d. For the linear specimens, these cumulative distributions are clearly linked to the \(PSDs\); as the \({C}_{u}\) increases the distribution becomes broader. Comparing Fig. 15d to Fig. 15a–c, it is clear that there are clear similarities between the shapes of \({CSD}^{stiffness}\) and its \(PSD\), \({PSD}^{stress}\), and \({CSD}^{stress}\). This suggests that the contribution of each individual contact to the overall stiffness relates to its contribution to the overall stress. In addition, the stiffness transferred by each individual particle may also be proportional to its volume fraction for linear specimens.
Data equivalent to those shown in Fig. 15 are presented in Fig. 16 for the gap-graded specimens. Figure 16a–d present the results for the SR of 3.7, while Fig. 16e–h show the results for the SR of 8.4. The contribution of contacts in each of the three sub-networks in a bimodal specimen can also be isolated. Figure 17a and b show that for the SR of 3.7, the contribution of the \(F-F\) contacts to the overall stiffness is negligble when \({F}_{finer}\le 15\%\), and subsequently increases with increasing \({F}_{finer}\), while the contribution of the \(C-C\) contacts to the overall stiffness decreases with increasing \({F}_{finer}\). In contrast, the contribution from the \(C-F\) contacts increases significantly and reaches approxmately 65% when \({F}_{finer}\) is 50%. For the \(SR\) of 8.4 (Fig. 17c, d), a different behaviour is observed when \({F}_{finer}\le 20\%\), where both the \(F-F\) and \(C-F\) contacts have a negligible contribution to the overall stiffness at all packing densities. Figure 17c and d also indicates that the \(C-F\) have a contribution of 80% to the overall stiffness when \({F}_{finer}\) is approximately 50%. These stiffness distribution data clearly indicate that different classes of contact make a distinct contribution to the stiffness, which again supports the idea that particle scale stress distribution may significantly affect the macro scale stiffness of gap-graded soils. These data put into doubt whether \({Z}_{m}\) and \({e}_{m}\) are relative measures of state to predict the behaviour of mixtures, since these two parameters consider all active contacts and grains as to be equivalent.
For the trimodal specimens, there are six different types of contact: coarse-coarse contacts (\(C-C\)); coarse-intermediate contacts (\(C-I\)); coarse-finer contacts (\(C-F\)); intermediate-finer contacts (\(I-F\)); intermediate-intermediate (\(I-I\)); finer-finer contacts (\(F-F\)). Figure 18a and c shows the distribution in the proportion of stress transmitted by these different contact classes for sample \(Tri 25\_15\) and \(Tri 25\_45\), respectively. While Fig. 18b and d illustrates the distribution of the contribution to the overall stiffness amongst the different contact types for these two samples. Differences between \({CSD}^{stress}\) and \({CSD}^{stiffness}\) can be observed. For instance, for \(Tri 25\_15\) in the dense condition, the \(C-F\) contacts transfer approximately 34% stress while the contribution of the \(C-F\) contacts to the overall stiffness is approximately 66%. A significant density effect is also observed for both the \(Tri 25\_15\) and \(Tri 25\_45\) specimens in considering both the stress and stiffness data. This strong density effect is similar to that observed for bimodal gap-graded soils, which may be one of the key characteristics for gap-graded soils.
Measure of state that accounts for heterogeneity in stress transmission
As discussed above, active finer and coarse particles are given equal weighting in the calculation of \({e}_{m}\), while referring to Fig. 12, the \(C-C\) contacts are much stiffer. Accepting that the general framework proposed by Hardin & Richart [6] is valid, we empirically explored a measure of state in which the contribution of different contacts or particles is weighted. Identifying a contact-based measure of state is nontrivial, contacts are not associated with a volume. Consequently, we focussed on developing a rational measure of state that weights the contribution of the particles by the stress they transmit by adopting the stress reduction factor \(\alpha\) proposed in Shire et al. [33]. Following Shire et al. [33], this factor quantifies the stress contribution amongst the different particle size fraction and it is used here to weight the contribution of the finer or coarse fraction in a modified void ratio, we term \({e}_{\alpha }\). When \(\alpha \le 1\) the relative contribution of finer fraction is lower than its volume fraction, the stress reduction factor of finer fraction, \({\alpha }_{f}\) can be then estimated as below:
$${p}_{finer}^{\mathrm{^{\prime}}}={\alpha }_{f}{p}^{\mathrm{^{\prime}}}$$
(25)
$${p}_{finer}^{\mathrm{^{\prime}}}=\frac{(1-{n}_{p})}{\sum_{{N}_{p,finer}}{V}^{a}}\sum_{a=1}^{{N}_{p,finer}}({p}^{a}{V}^{a})$$
(26)
The \(p_{{{\text{finer}}}}^{\prime }\) is the effective stress transferred by the finer fraction, \({n}_{p}\) is specimen porosity, \({N}_{p,finer}\) is the number of active finer particles. The new measure of state is then given as:
$$e_{\alpha } = \frac{{V_{t} - \left( {V_{c} + \alpha_{f} V_{f} } \right)}}{{\left( {V_{c} + \alpha_{f} V_{f} } \right)}}$$
(27)
where the \({V}_{t}\) is the total volume of specimen, the \({V}_{c}\) is the volume of active coarse grains, the \({V}_{f}\) is the volume of active finer grains. While when \({\alpha }_{f}\ge 1\), as illustrated in Shire et al. [33], the material is overfilled, the stress contribution of finer fraction is larger than its volume fraction. The stress contribution of coarse fraction is smaller than its volume fraction in this case. The stress reduction factor \({\alpha }_{c}\) is therefore proposed to reflect this case.
$${p}_{coarse}^{^{\prime}}={\alpha }_{c}{p}^{^{\prime}}$$
(28)
$${p}_{coarse}^{\mathrm{^{\prime}}}=\frac{(1-{n}_{p})}{\sum_{{N}_{p,coarse}}{V}^{a}}\sum_{p=1}^{{N}_{p,coarse}}({p}^{a}{V}^{a})$$
(29)
and the new measure of state is defined as:
$$e_{\alpha } = \frac{{V_{t} - \left( {\alpha_{c} V_{c} + V_{f} } \right)}}{{\left( {\alpha_{c} V_{c} + V_{f} } \right)}}$$
(30)
The \({e}_{\alpha }\) can be estimated from Eqs. (27) and (30). Figures 19a and b show the variation in \({\alpha }_{f}\) and \({\alpha }_{c}\) with \({F}_{finer}\) for \(SRs\) of 3.7 and 8.4, respectively. When \(SR\) = 3.7, \({\alpha }_{f}\) values remain approximately equal to 0.25 when \({F}_{finer}\le 20\%\). In contrast, when \(SR\) is 8.4, the \({\alpha }_{f}\) values are close to 0 when \({F}_{finer}\le 20\%\); this observation holds for \(SR\) values of 14.5 and 18.1. Then the \({\alpha }_{f}\) values increase with increasing \({F}_{finer}\). The \({\alpha }_{c}\) values are also presented in Fig. 19; for instance, in the dense condition (\(SR=8.4)\), when \({F}_{finer}\) is 35% and 50%, the stress transferred by the coarse fraction is lower than its volume fraction, the \({\alpha }_{c}\) rather than \({\alpha }_{f}\) is then presented in Fig. 19b.
Figure 20a illustrates the variation in \({G}_{0}\) with \({e}_{\alpha }\) for all the specimens with \(SR\) = 8.4 at the \({\sigma }_{3}^{^{\prime}}\) of 500 \(kPa\), the correlation can be approximated relatively well by a straight line with \({R}^{2}\) \(\approx\) 0.91. In contrast, the correlations were much weaker when \(e\) (\({R}^{2}\approx 0.27\)) and \({e}_{m}\) (\({R}^{2}\approx 0.80\)) were considered (subsets of the data on Fig. 7). Figure 21a shows that the relationship between \({e}_{\alpha }\) and \({Z}_{m}/(1+{e}_{m})\) is linear (for \({R}^{2}\) = 0.92) considering all the bimodal and trimodal specimens. For the trimodal specimens, the active coarse and intermediate fractions are combined to estimate \({e}_{\alpha }\). Figure 21b also show that a reasonable fit data is obtained using \({e}_{\alpha }\) as the state variable in Eq. (2) and taking \(n=0.33\). These results clearly indicate that the distribution of stress amongst the different size fractions has a significant influence on \({G}_{0}\) in the case of gap-graded soils.