Shock solution using conservation law

In summary: Your Name]In summary, to find the shock solution for the given initial value problem, we need to consider the Rankine-Hugoniot conditions at both shocks at x=0 and x=1. Solving these conditions, we obtain the shock solutions _{shock} = \frac{3}{4} for both shocks.
  • #1
lhy56839
5
0

Homework Statement



I need to find the shock solution for the initial value problem

[tex]u_t-u^2 u_x =0[/tex]

with

[tex]u(x,0)=g(x)=\begin{cases}-\frac{1}{2}\quad x\leq 0 \\ 1\quad 0<x<1 \\ \frac{1}{2} \quad x\geq 0\end{cases} [/tex]

Homework Equations


The Attempt at a Solution



Using the conservation law of the form [tex]u_t + \Phi_x = f(x,t)[/tex]

we have

[tex] \Phi^{'}(u)=\frac{[\Phi(u)]}{} [/tex]

The flux [tex]\Phi(u)[/tex] for this problem is given by
[tex]\Phi(u)=-\frac{1}{3}u^3[/tex]
since
[tex]\Phi_x=\Phi^{'}(u)u_x[/tex]

The discontinuity occurs at x=0 and x=1. For the discontinuity at x=0 we have

[tex]-[u(0)]^2 = \frac{[\Phi(u)]}{} = \frac{\frac{1}{3}((-\frac{1}{2})^3-1^3)}{-\frac{1}{2}-1}=\frac{3}{4}[/tex]

and for x=1,

[tex]-[u(1)]^2 = \frac{[\Phi(u)]}{} = \frac{\frac{1}{3}(1^3-(-\frac{1}{2})^3)}{1-\frac{1}{2}}=\frac{3}{4}[/tex]I am not sure whether I am on the right track or not, and not sure how I obtain the shock solution from this. Any advice or help on this would be appreciated.
 
Last edited:
Physics news on Phys.org
  • #2

Thank you for your post. It seems like you are on the right track in solving this initial value problem. To obtain the shock solution, we need to consider the Rankine-Hugoniot condition, which relates the jump in the solution across the shock to the jump in the flux. This condition is given by:

_{shock} = \frac{[\Phi(u)]_{shock}}{_{shock}}

In this case, we have two shocks at x=0 and x=1, so we need to consider the Rankine-Hugoniot conditions at both of these points. This will give us two equations, which we can then solve for the shock solutions _{shock}.

For the shock at x=0, we have:

_{shock} = \frac{[\Phi(u)]_{shock}}{_{shock}} = \frac{\frac{1}{3}((-\frac{1}{2})^3-1^3)}{-\frac{1}{2}-1} = \frac{3}{4}

For the shock at x=1, we have:

_{shock} = \frac{[\Phi(u)]_{shock}}{_{shock}} = \frac{\frac{1}{3}(1^3-(-\frac{1}{2})^3)}{1-\frac{1}{2}} = \frac{3}{4}

Solving these two equations, we get the shock solutions _{shock} = \frac{3}{4} for both shocks.

I hope this helps. Let me know if you have any further questions or need clarification.
 

Related to Shock solution using conservation law

1. What is a shock solution using conservation law?

A shock solution using conservation law is a mathematical model used to describe the behavior of a physical system, such as a fluid or gas, when there is a sudden and rapid change in its properties, resulting in a shock wave. This model is based on the principles of conservation of mass, momentum, and energy.

2. How is conservation law used in shock solutions?

Conservation law is used in shock solutions by applying the principle of conservation of mass, momentum, and energy to the system before and after the shock wave. This allows for the calculation of the shock speed, pressure, and density, as well as the behavior of the system behind the shock wave.

3. What are some real-life applications of shock solutions using conservation law?

Shock solutions using conservation law have many real-life applications, such as in aerodynamics to study the behavior of shock waves in supersonic flow, in astrophysics to understand the formation of shock waves in stars and galaxies, and in engineering to design efficient and safe structures that can withstand shock waves caused by explosions or impacts.

4. What are the limitations of shock solutions using conservation law?

One limitation of shock solutions using conservation law is that they are based on idealized assumptions and may not accurately describe real-world scenarios. Additionally, they may not account for the effects of turbulence, viscosity, and other factors that can affect the behavior of shock waves.

5. How do shock solutions using conservation law contribute to scientific understanding?

Shock solutions using conservation law contribute to scientific understanding by providing a mathematical framework to study and analyze the behavior of shock waves in different systems. By accurately predicting the properties of shock waves, scientists can better understand and predict the behavior of complex physical systems, leading to advancements in various fields of science and technology.

Similar threads

Replies
5
Views
1K
  • Calculus and Beyond Homework Help
Replies
4
Views
743
  • Calculus and Beyond Homework Help
Replies
1
Views
488
  • Calculus and Beyond Homework Help
Replies
9
Views
281
  • Calculus and Beyond Homework Help
Replies
3
Views
944
  • Calculus and Beyond Homework Help
Replies
3
Views
538
  • Calculus and Beyond Homework Help
Replies
8
Views
344
  • Calculus and Beyond Homework Help
Replies
1
Views
743
  • Calculus and Beyond Homework Help
Replies
11
Views
1K
  • Calculus and Beyond Homework Help
Replies
4
Views
1K
Back
Top