Shooting method and a shock wave (discontinuity at the inner boundary condition)

AI Thread Summary
The discussion focuses on using a shooting method to solve steady-state spherically symmetric fluid equations for an accreting plasma, specifically addressing challenges related to unknown inner boundary conditions at the sonic transition radius. The issue arises from a division by zero in the equations at this boundary. The inquiry seeks guidance on whether L'Hopital's rule is sufficient for initial iterations or if a Taylor expansion is necessary for smooth integration near the inner boundary. Responses highlight that both L'Hopital's rule and Taylor expansions can be effective, but the choice depends on the required accuracy. Additionally, exploring various integration methods, such as higher-order techniques like Runge-Kutta or Adams-Bashforth, is recommended for improved results. The sensitivity of numerical solutions to initial conditions and parameters is also emphasized, suggesting careful selection of these elements to ensure consistency with the physical system being modeled.
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I've done searching on the topic, and I really don't know where else to turn, so here it goes. I hope somebody can point me in the right direction.

I've been working on using a shooting method to solve the steady-state spherically symmetric fluid equations for an accreting plasma. Basically, it boils down to solving a system of coupled nonlinear ordinary differential equations. The inner boundary conditions are unknown, and I'm using a shooting method to match the outer boundary conditions.

The inner boundary condition for the three unknowns is at the sonic transition radius for the inward flowing gas. At this point, there is division by zero in one of the equations. Let's say the equation is of the form \frac{vdv}{dr} = \frac{A}{B}. So, at this inner boundary condition B = 0. Now, based on the condition that B = 0, it must be required that A = 0, and from A = 0, we get another of the inner boundary conditions. Now, this may be a stupid question, but is it typically sufficient to use something really basic like L'Hopitals rule to handle the first few iterations through the integration out to a radius of let's say within 0.1 percent of the sonic radius. Or is it required to use some kind of taylor expansion and keep quite a few terms to achieve smooth integration near the inner boundary condition.

I hope the question is clear enough. Thanks in advance for any help.
 
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Thank you for reaching out for help with your research. I can understand the challenges you are facing in solving the steady-state spherically symmetric fluid equations for an accreting plasma.

Firstly, I would like to commend you for using the shooting method to solve the system of coupled nonlinear ordinary differential equations. This is a common and effective approach for solving such problems.

Regarding your question about handling the division by zero at the inner boundary condition, using L'Hopital's rule or a Taylor expansion can be viable options. However, it ultimately depends on the specific problem and the accuracy required for your solution. In some cases, a simple linear interpolation or extrapolation method can also work well. I would suggest trying out different methods and comparing the results to see which one gives the most accurate and stable solution.

Another important aspect to consider is the choice of your integration method. Depending on the nature of your equations, using a higher-order integration method such as Runge-Kutta or Adams-Bashforth can help in achieving smoother and more accurate results near the inner boundary condition.

It is also worth mentioning that solving the equations numerically can be sensitive to initial conditions and small changes in the parameters. Therefore, it is important to carefully choose your initial conditions and ensure that they are consistent with the physical properties of the system.

I hope this helps in pointing you in the right direction. If you have any further questions or need any assistance, please do not hesitate to ask. Good luck with your research.
 
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