# 9.5.1 Raman’s bowed-string model

For an ideal flexible string, obeying the wave equation as derived in section 3.1.1, the equations governing the motion in response to bowing at a single point take a rather simple form. If the ends of the string are either rigid, or terminated by dashpots, the reflection functions used in the travelling-wave model derived in section 9.2.1 take the form of Dirac delta functions. There is no “corner-rounding”. For a rigid end, the delta function has amplitude $-1$, whereas for a dashpot termination it has a negative magnitude $\lambda$ with $|\lambda| < 1$. The reflection coefficient $\lambda$ is determined by the impedance ratio of the string and the dashpot as we showed in equation (5) of section 5.1.2: provided the impedance ratio $Z_{0}/Z_{body} \ll 1$, $\lambda \approx -1 + 2Z_{0}/Z_{body}$.

Now an important simplification occurs if the bowing position $\beta$ is a ratio $p/q$ of two integers. We can define a time interval $\Delta=T/(p+q)$ where $T$ is the round-trip period for transverse waves on the string. Reflections only arrive back at the bowed point at times that are multiples of $\Delta$, so both the force and velocity at the bowed point can only change at times $t=n\Delta$. In other words, provided the initial conditions are consistent with this pattern, both the force and velocity waveforms consist of steps of length $\Delta$ during which they stay constant, separated by jumps.

We can define these constant levels to be $v_n=v(n \Delta)$ and $f_n=f(n \Delta)$. The model development then follows the general treatment in section 9.2.1, but the convolution operations become very simple because both reflection functions are delta functions. If for simplicity we assume that both ends of the string have the same value of $\lambda$, then for example $(r_1 * f)_n = \lambda f_{n-p}$ and $(r_2 * f)_n = \lambda f_{n-q}$. After a little algebraic manipulation, the resulting equation can be cast into a difference equation

$$v_n – \lambda^2 v_{n-N} = \dfrac{1}{2Z_0} \left[f_n + \lambda f_{n-p} + \lambda f_{n-q} + \lambda^2 f_{n-N} \right] \tag{1}$$

where $N=p+q$. As usual, for each successive value of $n$ this equation is to be solved simultaneously with

$$f_n = F_b \mu(v_n) \tag{2}$$

where $F_b$ is the bow force and $\mu(v)$ is the friction coefficient.

The simplicity of this model allows various mathematical investigations to be carried out relatively straightforwardly. Raman was able to solve the model for simple cases of periodic solutions, working by hand in the pre-computer era . Friedlander was able to study the stability of periodic solutions . For the case without losses, $\lambda =-1$, he proved a striking result. He first imposed the condition that the state of steady sliding is unstable, based on the observation that it is virtually impossible to draw a bow across a string without some vibration occurring. He showed that this condition is enough to make all periodic solutions unstable! However, when $|\lambda| < 1$ so that there is some energy dissipation, it becomes possible for periodic solutions like Helmholtz motion to be stable while steady sliding is still unstable .

We can illustrate some simple periodic solutions. Suppose we look for solutions with the natural period of the string, so that $v_{n+N}=v_n$ and $f_{n+N}=f_n$ for all values of $n$. Equation (1) then becomes

$$2 Z_0 (1 – \lambda^2) v_n = (1+ \lambda^2)f_n + \lambda f_{n-p} + \lambda f_{n-q} \tag{3}$$

except that when $n-p$ or $n-q$ go outside the range $1,\cdots,N$ they are folded back into that range by adding or subtracting a suitable multiple of $N$. The result is a set of $N$ simultaneous equations that can be written in the form

$$2 Z_0 (1 – \lambda^2) \mathbf{v} = M \mathbf{f} \tag{4}$$

where $\mathbf{v}$ and $\mathbf{f}$ are length-$N$ vectors containing the values of $v_n$ and $f_n$, and the matrix $M$ is given by

$$M=\begin{bmatrix}1+\lambda^2 & 0 & \cdots & \lambda & \cdots & \lambda & 0 & \cdots & 0\\0 & 1+\lambda^2 & 0 & \cdots & \lambda & \cdots & \lambda & 0 & \cdots \\ \vdots & \vdots & \vdots & \vdots & \vdots & \vdots & \vdots & \vdots & \vdots\\ \vdots & \vdots & \vdots & \vdots & \vdots & \vdots & \vdots & \vdots & \vdots \\\cdots & 0 & \lambda & \cdots & \lambda & \cdots & 0 & 1+\lambda^2 & 0\\0 & \cdots & 0 & \lambda & \cdots & \lambda & \cdots & 0 & 1+\lambda^2 \end{bmatrix} \tag{5}$$

where the diagonal bands containing $\lambda$ are spaced $p$ and $q$ places above and below the leading diagonal.

During an interval of sticking, we know that $v_n=v_b$, the bow speed, while the corresponding $f_n$ is unknown. The situation is reversed during an interval of slipping: now $v_n$ is unknown, but $f_n$ is determined by the assumed friction curve. Under the simplest assumption in which the coefficient of sliding friction is a constant value $\mu_d$, we have $f_n=F_b \mu_d$ where $F_b$ is the bow force. So to find solutions to equation (4), we decide which values of $n$ correspond to sticking, and which to slipping. Let us seek solutions looking like Helmholtz motion: in that case, we can say that for the first $q$ values we are sticking, while for the remaining $p$ values we are slipping. Now we partition the vectors and the matrix in this $q:p$ ratio:

$$\mathbf{v}=\begin{bmatrix} \mathbf{v_1}\\ \mathbf{v_2}\end{bmatrix},~~~\mathbf{f}=\begin{bmatrix} \mathbf{f_1}\\ \mathbf{f_2}\end{bmatrix}, M=\begin{bmatrix} A & B \\ C & D\end{bmatrix} \tag{6}$$

where $\mathbf{v_1}$ contains $q$ repeats of the value $v_b$, $\mathbf{v_2}$ contains the unknown velocities, $\mathbf{f_1}$ contains the unknown forces, and $\mathbf{f_2}$ contains $p$ repeats of the value $F_b \mu_d$.

Expanding the partitioned problem out we obtain

$$2 Z_0 (1 – \lambda^2) \mathbf{v_1}=A \mathbf{f_1}+B\mathbf{f_2} \tag{7}$$

and

$$2 Z_0 (1 – \lambda^2) \mathbf{v_2}=C \mathbf{f_1}+D\mathbf{f_2} . \tag{8}$$

Thus the unknown values are given by

$$\mathbf{f_1}=A^{-1} \left[ 2 Z_0 (1 – \lambda^2) \mathbf{v_1} – B\mathbf{f_2} \right] \tag{9}$$

and then

$$\mathbf{v_2}=\dfrac{1}{2 Z_0 (1 – \lambda^2)} \left[C \mathbf{f_1}+D\mathbf{f_2} \right] . \tag{10}$$

Figure 1 shows some computed examples. The first plot shows the force and velocity waveforms for the case $p=1$, $q=12$. Cases like this, where $\beta=1/(q+1)$ for some integer $q$, give the simplest possible examples. Raman and Guettler both made extensive use of such cases in their work. In order to show the effect of energy dissipation clearly, the rather unrealistic value $\lambda=-0.97$ has been chosen. The force waveform (in blue) shows the expected “staircase” structure, in an arch shape which is familiar to us from the discussion of the minimum bow force in section 9.3.1. The largest value of friction force occurs in the middle of the arch, and the condition that this should not be big enough to cause a second slip at that moment is what led Raman, and later Schelleng, to the criterion for minimum bow force. Figure 1. Examples of periodic solutions to the Raman model, all with $\beta$ close to 1/13. Top left: $p=1$, $q=12$; top right: $p=3$, $q=37$; bottom left: $p=5$, $q=61$; bottom right: $p=5$, $q=59$. In each case the red curve shows two cycles of the velocity waveform, while the blue curve shows the friction force waveform. The value of $\lambda=-0.97$ throughout.

The other plots in Fig. 1 show cases with very similar values of $\beta$, but involving larger numbers of steps in the staircase waveforms. The top right plot shows $p=3$, $q=37$. There are now three steps in the slipping interval, and the force waveform is a little more complicated, although still showing the underlying arch shape clearly. The two plots in the bottom row show values of $\beta$ on either side of the value 1/13. It can be seen that the small changes in the slipping velocity waveform behave in opposite ways in these two cases.

 C. V. Raman: “On the mechanical theory of the vibrations of bowed strings and of musical instruments of the violin family, with experimental verification of the results. Part I.” Indian Association for the Cultivation of Science Bulletin 15, 1–158 (1918).

 F. G. Friedlander: “On the oscillations of a bowed string”, Proceedings of the Cambridge Philosophical Society, 49, 516–530 (1953).

 J. Woodhouse: “On the stability of bowed-string motion”; Acustica, 80, 58–72 (1994).