We have set the grid points in our stencil along x plane. each grid points have its own taylor series functions. we have to create a taylor table from these sets of grid points 1.Fourth order approximation of second order derivative using Central difference method: `Deltax^2(d^2f)/dx^2=a*f(i-2)+b*f(i-1)+c*f(i)+d*f(i+1)+e*f(i+2)`…

STEADY STATE: we have to solve the study state equation using different iterative solvers.they are, Jacobi method. Gauss-seidel method. Successive over relaxation method. Heat Conduction equation is ,  `(del^2T)/(delx^2)+(del^2T)/(dely^2)=0` by discretize the above equation we get, `T_P^(n+1)=1/K[(T_L+T_R)/(Deltax^2)+(T_B+T_T)/(Deltay^2)]^n`--------(a)…

Convergent divergent nozzle or the supersonic nozzle or the delaval nozzle is used for supersonic flows. This has three sections: Subsonic section, throat, supersonic section.    Fluid of low subsonic speed enter the subsonic section and the speed increases to the high subsonic speed at the end of the section.…

Considering a 2D laminar, incompressible and Newtonian fluid flow over the Backward-facing step with given kinamatic viscosity as `10^-5 m/s`. Considering the 'No-slip boundary condition' on every wall under the domain. For the results, we need to perform simulations for given grading factors. We need to change the time…