The following reactor models include one-dimensional grids for steady-state solution:
Premixed Laminar Burner-stabilized Flame
Premixed Laminar Flame-speed Calculation
Opposed-flow Diffusion Flame
Premixed Burner-Stabilized Stagnation Flame
Flame-Extinction Simulator
Stagnation-flow CVD Reactor
Rotating-disk CVD Reactor
The numerical solution procedure begins by making finite difference approximations to reduce the boundary value problem to a system of algebraic equations. The initial approximations are usually on a very coarse mesh that may have as few as five or six points. After obtaining a solution on the coarse mesh, new mesh points are added in regions where the solution or its gradients change rapidly. We obtain an initial guess for the solution on the finer mesh by interpolating the coarse mesh solution. This procedure continues until no new mesh points are needed to resolve the solution to the degree specified by the user. This continuation from coarse to fine meshes has several important benefits that are explained later in this chapter. We attempt to solve the system of algebraic equations by the damped modified Newton algorithm in Twopnt. However, if the Newton algorithm fails to converge, the solution estimate is conditioned by integration in time. This provides a new starting point for the Newton algorithm that is closer to the solution, and thus more likely to be in the domain of convergence for Newton’s method. As the mesh becomes finer we normally find that the estimate interpolated from the previous mesh is within the domain of convergence of Newton’s method. This point is key to the solution strategy.