Physics problem: cumulative shell colliding with an armoured wall

Introduction and problem statement

This problem, as many others appearing here, took me a lot of time to wrap my head around. I almost lost faith, even tried to ask ChatGPT to solve it for me few times, but ChatGPT's solution was wrong or completely obscure for me.

Here is the problem statement (translated by ChatGPT from the Savchenko et al 1981 book).

Problem statement: In 1941, the Germans invented a cumulative anti-tank shell. The shell has a fuse on its front part, which, upon impact, causes detonation and ignites the entire charge. The shell penetrates the armor. In 1944, such German shells came into the hands of both the Soviets and their allies. Extensive experiments began. Various additional effects and paradoxes were discovered. The researchers started to investigate what exactly was penetrating the armor. At first, they thought it was a jet of hot gas that burns through the armor. However, it turned out that a metal jet is piercing through the armor traveling in a very puzzling way: in front of the plate at a speed of $v_{0} = {\rm 8\;km/s}$, inside the plate at ${\rm 4\;km/s}$, and behind the armor plate again at ${\rm 8\;km/s}$.

Explain this phenomenon and determine the speed of the metal wall of the conical cavity covering the charge, given that the cone’s vertex angle is 30°.

I have to admit that the translation is pretty accurate.

• You might prefer to read the notebook version of the post here.
• Latex sources for the plots are available here.

Figure 1: Cross-section of cumulative shell heading towards the armoured wall.

Solution

The problem consists of two parts. The first one asks to explain the phenomenon and the second one asks to determine the speed of the collapsing conical wall that is separating the fuse and the explosive charge of the shell, this collapsing wall is forming the metal jet piercing through the armor. I'll proceed in the order I solved it initially, starting with the part 2.

Part 2

Let's determine the speed of the conical wall collapsing into the jet flowing onto the armor at a speed of $v_{0} = {\rm 8\;km/s}$ as shown in Fig. 2. We focus here only on the upper part of the conical wall cross-section ($AB$, see Fig. 1 as well).

The breaking moment for me here was to realize that the velocity of the conical wall is orthogonal to its surface ($\vec{v}$ in Fig. 2). Since it is collapsing under the pressure force of the gas/liquid created to the left of the cone surface after the explosion of the charge.

Figure 2: Cross-section of the upper part of the collapsing conical wall.

Let's consider a reference frame in which the cone material flows along the cone surface at speed $\vec{v}_1$. This reference frame is moving to the right at a horizontal speed $\vec{u}$, so that the following relation is satisfied:

\begin{equation} \vec{v} - \vec{u} = \vec{v}_1 \end{equation}

In this reference frame the horizontal part of the jet is moving at speed $\left|\vec{v}_1\right| = v_1$ (here and below we ommit the arrow to denote scalar variables). This is relatively easy to prove using energy conservation. In summary we have the following system of equations:

\begin{align} \begin{cases} \vec{v} - \vec{u} = \vec{v}_1\\ v_0 - u = v_1\\ \end{cases} \end{align}

From the triangle formed by the speed vectors in Fig. 2 we get: \begin{align} \begin{cases} v_1 = v / \tan\left(\frac{\alpha}{2}\right)\\ u = v / \sin\left(\frac{\alpha}{2}\right) \end{cases} \end{align}

Now using the last two equations and the relation $v_0 - u = v_1$ we get an equation with respect to $v$:

\begin{align*} v_0 - u = v_1 & \Rightarrow v_0 - v / \sin\left(\frac{\alpha}{2}\right) = v / \tan\left(\frac{\alpha}{2}\right) \\ &\\ & \Rightarrow \boxed{v = \frac{v_0 \sin\left(\alpha/2\right)}{1 + \cos\left(\alpha/2\right)}}\\ &\\ & \Rightarrow v\approx 1.05\:{\rm km/s} \end{align*}

Part 1

The first part of the problem is to explain the phenomenon, mainly why the speed decreases by a factor of two in the armor. It is more or less clear that the jet will slow down due to the friction with the armor and then will accelerate back behind the armoured wall to the initial speed as it is being pushed forward. The factor of two for the velocity can be explained by the size of the hole pierced by the jet in the armoured wall (as shown in Fig. 3) which is two times larger than the diameter of the jet.

Figure 3: Metallic jet formed from the collapsed conic wall after piercing through the armoured wall, after the stationary flow regime is established.

So now we need to explain why the hole would be approximately twice the size of the metall jet piercing through the armor. For this we need to consider the moments before the hole is pierced completely. At this point there is a part of the jet that flows backwards reflected from the armor as shown in Fig.4 below, which expands the hole. The symmetry and mass conservation would hint us towards the factor of two for the hole diameter.

There is however a question, why would the backflow velocity be directed exactly in the opposite direction with respect to the incident jet. Indeed, this is not obvious.

Figure 4: Metallic jet formed from the collapsed conic wall prior to piercing through the armoured wall.

To find the angle at which the backward flow is reflected we can consider two colliding jets of liquid: smaller with a radius $r$ and a larger one with a radius $R$, moving towards each other at equal and parallel speeds (we can always switch to the reference frame where the metallic jet and the armoured wall move at equal speeds towards each other). As a result of the collision of the jets, a conical backflow in the direction of the smaller jet is formed. If we denote the angle of the cone as $2\beta$, then using momentum, mass and energy conseration it is relatively easy to show that the angle of the cone can be computed using dimensions of the colliding jets as follows: \begin{equation} \cos\beta = \frac{R^2-r^2}{R^2 + r^2} \end{equation}

Now, for our problem if we take the radius of the metallic jet to be $r$, it is much smaller than the effective radius of the armoured wall:

\begin{align} r \ll R & \Rightarrow \cos\beta = \frac{R^2-r^2}{R^2 + r^2} \approx 1 \\ & \Rightarrow \beta \approx 0 \end{align}

which means that indeed in our case the backflow is directed antiparallel to the incident jet velocity.

i3 (EndeavouOS edition): Multiple keyboard layouts

Here I will show you how to add a ukrainian keyboard layout to an existing layout (in this case us), so you can type using different languages.

• First add the following to your ~/.config/i3/config file:

  # add layouts
  exec setxkbmap -layout us,ua
  # set a switching shortcut
  exec setxkbmap -option 'grp:alt_shift_toggle'
  

• Now we want to show the current layout in the system tray (this might be distribution dependent, I guess). EndeavourOS provides some ready scripts for which I needed to install dependencies and uncomment some lines in the ~/.config/i3/i3blocks.config.
  • Install dependencies

    yay xkblayout-state
    

  • Uncomment the following block in ~/.config/i3/i3blocks.config:

    [keyboard-layout]
    command=~/.config/i3/scripts/keyboard-layout
    interval=2
    

Here is the screenshot of the way my env looks right now.