Appendix A: Mechanism and Location of Dissipation: Arguments for Linear Scaling of Dissipation Rate with Contact Size
The main, but not sole mechanism (see below) of mechanical energy dissipation in friction force microscopy is related to the rapid motion of the tip apex with respect to the surface. It is accompanied by the creation of phonons in the substrate and in the tip. These phonons lead to the dissipation (irretrievable loss) of energy [19], and result (at a later stage) in thermalization. As mentioned in the main text, damping of the motion of an adsorbed atom on a surface is always close to critical. In the case of a sharp tip that is in contact with the surface via one single atom, phonons are produced not only in the substrate but also in the tip. As a result, the dissipation rate will then be higher than in the adsorbed-atom case by at most a factor two.
In this study, we have assumed the total dissipation rate, experienced when the tip apex is blunt, simply to be proportional to number of atoms in contact \({N_{{\text{cont}}}}\) (see Eq. 3). A justification for this can be given at more than one level. Obviously, if we consider each atom in the contact as a separate, independent (Einstein) oscillator that is vibrationally excited in the slip process and dissipates that vibrational energy independently, our model automatically exhibits the linear scaling of Eq. 3.
In a more realistic description, the \({N_{{\text{cont}}}}\) contacting atoms are treated as coupled oscillators, rather than independent ones. The total number of vibrational modes introduced by these atoms amounts to \(3{N_{{\text{cont}}}} - 6\), which is nearly proportional to the contact size. If, on average, each of these modes contributes equally strongly to the energy dissipation, this description still results in near-linear scaling, very close to Eq. 3.
Of course, the vibrations that are relevant here are not limited to the \({N_{{\text{cont}}}}\) contact atoms, but also involve nearby tip atoms that are not in contact with the counter-surface themselves. As a result, more than \(3{N_{{\text{cont}}}} - 6\) modes will be involved and the effective number of modes contributing to the dissipation should scale super-linearly with \({N_{{\text{cont}}}},~\)for example approximately proportional to \(N_{{{\text{cont}}}}^{{{\raise0.7ex\hbox{$3$} \!\mathord{\left/ {\vphantom {3 2}}\right.\kern-0pt}\!\lower0.7ex\hbox{$2$}}}}\) (under the assumption that the aspect ratios of the tip dimensions are all constant). Such an alternative scaling will lead to modifications in the powers of \({N_{{\text{cont}}}}\) in Eqs. 3 and 4 (3/2 and 3, respectively, instead of 1 and 2) and a change in the horizontal axis of Fig. 4.
We should also mention the phonon discrimination mechanism that was proposed in [23] to explain surface diffusion of atomic clusters. Surface motion of a large (rigid) object can couple only to phonons in the substrate that have wavelengths that are comparable to or larger than the lateral size of the object. This discrimination effect actually leads to sublinear scaling with the size as \(\sqrt {{N_{{\text{cont}}}}}\). Combining this sublinear tendency with the super-linear tendency mentioned in the previous paragraph, we may expect the naïve, linear scaling to provide a useful order-of-magnitude estimate.
We close this part by emphasizing that, in view of the low values of \({N_{{\text{cont}}}}\), considered here, the numerical effects of any non-linearity will necessarily be modest and the qualitative conclusions reached in this article should remain valid.
For completeness, also more ‘remote’ channels of mechanical energy dissipation may be active in friction force microscopy. For example, the cantilever may exhibit internal damping. Since the quality factors measured for free cantilevers are typically in the order of thousands [14], this internal damping must be negligibly weak. Similarly, the internal damping of the bending motion of the tip or its apex must be insignificant, since the quality factors measured for cantilevers with the tip in contact with a substrate are still relatively high, in the order of hundreds [14]. These observations justify the choice in our calculations not to introduce explicit damping in Eqs. 7 and 8 (see Appendix B), and not to include terms depending on the relative velocity of the tip apex and the cantilever in Eqs. 5 and 6. Note that Eqs. 5–8 do imply modest, indirect damping of the cantilever via the slow, forced motion of the tip with respect to the substrate; this effect is smaller than the explicit damping of the rapid mode by a factor \({m_{{\text{dyn}}}}/{m_{{\text{cant}}}}\).
Appendix B: Details of the Numerical Calculations
Equations of Motion
In our calculations, we numerically integrated the equations of motion for the dynamic tip mass, \({m_{{\text{dyn}}}},\) and of the combination of the rest of the tip and the moving part of the cantilever, \({m_{{\text{cant}}}}.\) Both were followed in two dimensions, leading to the following four coupled Langevin equations:
$${m_{{\text{dyn}}}}{\ddot {x}_{{\text{tip}}}}= - {\left. {\frac{{\partial {V_{{\text{int}}}}\left( {x,y} \right)}}{{\partial x}}} \right|_{\left( {x,y} \right)=\left( {{x_{{\text{tip}}}},{y_{{\text{tip}}}}} \right)}} - {k_{{\text{dyn}}}}\left( {{x_{{\text{tip}}}} - {x_{{\text{cant}}}}} \right)+{\xi _x} - \gamma {\dot {x}_{{\text{tip}}}},$$
(5)
$${m_{{\text{dyn}}}}{\ddot {y}_{{\text{tip}}}}= - {\left. {\frac{{\partial {V_{{\text{int}}}}\left( {x,y} \right)}}{{\partial y}}} \right|_{\left( {x,y} \right)=\left( {{x_{{\text{tip}}}},{y_{{\text{tip}}}}} \right)}} - {k_{dyn}}\left( {{y_{{\text{tip}}}} - {y_{{\text{cant}}}}} \right)+{\xi _y} - \gamma {\dot {y}_{{\text{tip}}}},$$
(6)
$${m_{{\text{cant}}}}{\ddot {x}_{{\text{cant}}}}= - {k_{{\text{cant}}}}\left( {{x_{{\text{cant}}}} - {x_{{\text{supp}}}}} \right) - {k_{{\text{dyn}}}}\left( {{x_{{\text{cant}}}} - {x_{{\text{tip}}}}} \right),$$
(7)
$${m_{{\text{cant}}}}{\ddot {y}_{{\text{cant}}}}= - {k_{{\text{cant}}}}\left( {{y_{{\text{cant}}}} - {y_{{\text{supp}}}}} \right) - {k_{{\text{dyn}}}}\left( {{y_{{\text{cant}}}} - {y_{{\text{tip}}}}} \right).$$
(8)
Note that Eqs. 7 and 8 have no damping and no noise term, which reduces them to straightforward Newton equations of motion. In our calculation, damping and noise exclusively derive from the tip–surface contact and are therefore only explicitly present in Eqs. 5 and 6. Here, the spring coefficients have been chosen equal for the x- and y-directions, but they can be replaced easily by an anisotropic choice. In our computational scheme, we numerically integrated these equations, using the Verlet algorithm to periodically update the four velocities, \({\dot {x}_{{\text{tip}}}},\) \({\dot {y}_{{\text{tip}}}}\), \({\dot {x}_{{\text{cant}}}},\) and \({\dot {y}_{{\text{cant}}}},\) and the four positions, \({x_{{\text{tip}}}},\) \({y_{{\text{tip}}}},\) \({x_{{\text{cant}}}},\) and \({y_{{\text{cant}}}},~\)iterating with a time step \({\text{d}}t\) [32].Footnote 1
Interaction Potential
The two-dimensional periodic potential \({V_{{\text{int}}}}\) describes the interaction between the tip apex and the crystal surface over which the tip is forced to slide. Here, we used a potential with the symmetry and lattice period of graphite, based on the potential that was used before by Verhoeven et al. [33 and references therein].
$${V_{{\text{int}}}}\left( {x,y} \right)= - \frac{2}{9}{U_0}\left[ {2{\text{cos}}\left( {{a_1}x} \right){\text{cos}}\left( {{a_2}y} \right)+{\text{cos}}\left( {2{a_2}y} \right)} \right]$$
(9)
with \({a_1}=2\pi /\left( {0.246~{\text{nm}}} \right)\) and \({a_2}=2\pi /\left( {0.426~{\text{nm}}} \right)\), determined by the periodicity of the graphite surface. The prefactor of \(2/9\) serves to make the peak-to-peak variation of \({V_{{\text{int}}}}\) equal to \({U_0}.\)
Time Step
For the time step \({\text{d}}t\) between subsequent iterations, we introduce two upper limits. On the one hand, \({\text{d}}t\) should be short enough to capture the behavior of the most dynamic element in the system, namely the dynamic tip. Therefore, we respect one upper limit for \({\text{d}}t\) as 10% of the vibrational period of the tip apex,
$${\text{d}}t_{1}^{{max}}=0.1 \cdot 2\pi \sqrt {\frac{{{m_{{\text{dyn}}}}}}{{{k_{{\text{dyn}}}}+{k_{{\text{latt}}}}}}},$$
(10)
in which \({k_{{\text{latt}}}}\) is the maximum force derivative by which the interaction potential contributes to the total spring constant, experienced by the tip apex.
The second constraint on the time step derives from the random force, generated via the noise terms \({\xi _x}\) and \({\xi _y}\) in Eqs. 5 and 6. In case of strong dissipation, the noise will be high too, as they are related via the fluctuation–dissipation theorem. Hence, the influence of the noise on the acceleration will be high and thus we need to choose an accordingly small time step. The characteristic timescale of the noise is set by the dissipation rate and the mass, and we verified that our numerical results are sufficiently reliable and stable when we keep \({\text{d}}t\) below 20% of this time, which defines our second upper limit as
$${\text{d}}t_{2}^{{{\text{ma}}x}}=0.2 \cdot \frac{{{m_{{\text{dyn}}}}}}{\gamma }.$$
(11)
We combine these two conditions into \(dt={\text{min}}\left( {dt_{1}^{{{\text{max}}}},dt_{2}^{{{\text{max}}}}} \right).\)
Noise Term
The noise term \(\xi\) in Eqs. 5 and 6 is provided in the calculations as a Gaussian-distributed, uncorrelated random number with a standard deviation in accordance with the fluctuation–dissipation theorem \(\left< {\xi \left( t \right)\xi \left( {t'} \right)}\right>=2\gamma {k_B}T\delta \left( {t - t'} \right)\), where \({k_B}\) is the Boltzmann constant. Actual \(\xi\)-values are generated in our calculations by means of regular, uniformly distributed random numbers and a Box–Muller transformation [34], in order to obtain a Gaussian distribution. We verified that this procedure indeed generates a Gaussian distribution of random forces, with an average of zero and a mean square value satisfying the fluctuation–dissipation theorem for the specific combination of temperature \(T\) and dissipation rate \(\gamma\) of the calculation.
Damping of the Cantilever
In the numerical calculations reported, no damping was applied to the cantilever. As typical cantilevers have very high-quality factors (thousands), even in contact (hundreds) [14], both the damping and the noise on the cantilever motion are relatively small (see also Appendix A). Calculations were performed to check this in case of a close-to-critically-damped tip apex and almost no effect on the dynamic tip apex behavior was observed at typical cantilever damping values. Taking confidence from these observations, we set the damping of the cantilever to zero in all calculations reported here, which resulted in a significant reduction in calculation time.
Scan Trajectory of the Support
In FFM-experiments, like in most scanning probe experiments, the support is scanned over the surface in a line-by-line fashion. In our calculations, we oriented our coordinate system such that the scan lines were oriented along the x-axis. Every combination of a forward and subsequent backward line was performed at a fixed y-coordinate of the support. Prior to the next forward–backward line pair, the support made a small step along the y-direction.
We have faithfully followed this scan sequence in our calculations, because it leads to a characteristic hysteresis in the lateral force maps, both along the x-direction and, after a few initial scan lines, also along the y-direction. For example, during the initial part of each forward line, the x-force first has to reduce to zero, change sign, and build up in the opposite direction to a level high enough to induce slip events. Such hysteresis is commonly observed in experiments [2] and is reproduced well by our calculations, indicating that not only the typical slip-induced force variations in the calculations are similar to those in experiments, but also the typical force level at which slip events take place.