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20                         2  Simulating Steady-State Natural Convective Problems

            864 nine-node quadrilateral elements of 3577 nodes in total. The mesh gradation
            technique, which enables the region in the vicinity of problem boundaries to be
            modelled using finite elements of small sizes, has been employed to increase the
            solution accuracy in this region. The following parameters associated with the pro-
                                                                        o
            gressive asymptotic approach procedure are used in the calculation: α = 5 , n = 2
            and R = 5.
              Figures 2.4, 2.5, 2.6 and 2.7 show the comparison of numerical solutions with
            analytical ones for dimensionless velocity, stream function, temperature and pres-
            sure modes respectively. In these figures, the plots above are analytical solutions,
            whereas the plots below are numerical solutions for the problem. It is observed from
            these results that the numerical solutions from the progressive asymptotic approach
            procedure associated with the finite element method are in good agreement with the
            analytical solutions. Compared with the analytical solutions, the maximum error in
            the numerical solutions is less than 2%. This demonstrates the usefulness of the
            present progressive asymptotic approach procedure when it is used to solve the
            steady-state Horton-Rogers-Lapwood problems.
              At this point, there is a need to explain why both the analytical and the numer-
            ical solutions for the pore-fluid flow are non-symmetric, although the geometry
            and boundary conditions for the problem are symmetric. As stated previously, the
            Horton-Rogers-Lapwood problem belongs mathematically to a bifurcation problem.
            The trivial solution for the pore-fluid flow of the problem is zero. That is to say, if
            the Rayleigh number of the problem is less than the critical Rayleigh number, the
            solution resulting from any small disturbance or perturbation converges to the trivial
































            Fig. 2.4 Comparison of numerical solution with analytical solution (Dimensionless velocity)
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