Lecture 17 Reactor Theory-II Objectives In this lecture you will learn the following In this lecture we shall look at cylindrical reactor. As the solution turns out to be a Bessel function, we shall briefly look at the nature of these functions. Finally we will show that the flux is more peaked for a cylindrical reactor than for a slab reactor. 1 2 3 4 5 6 /6 GO Lecture 17 Reactor Theory-II Reactor Theory Now we shall focus our attention towards cylindrical and spherical reactors. The governing equation shall continue to be where, 2 would be different for cylinder and sphere. The term for Cylindrical Reactor Let us now consider an infinite cylindrical reactor as shown From last slide, we can write the governing equation as 2 +B2 = 0. Note that we have replaced B m with B. For the Cylindrical case, the simplified equation shall be 1 2 3 4 5 6 /6 GO Lecture 17 Reactor Theory-II The solution for the above equation is Bessel’s Equation of order zero For those who are not familiar with the Bessel Functions, let us digress a bit and understand them. Notice that when a cylinder is large, the curvature effects are small and hence the solution of cylinder must look similar to the Cartesian case. Thus the functions J0 and Y 0 should be similar to Sine and Cosine. Bessel Functions 1 2 3 4 5 6 /6 GO Lecture 17 Reactor Theory-II Properties of Bessel Function Note that both J0 and Y 0 are oscillating functions with decaying amplitude. The reason for the decay in amplitude can be attributed to the divergence of the coordinate in r direction. Similar to Sine and Cosine, they have multiple roots. The first root of J0 is 2.405. There are some properties of J0 and Y 0 which we shall describe below Y 0(0) = -∞ J0(0) = 1 First root of J0 is 2.405, That is J0 (2.405) = 0. Another property of J0 is that 1 2 3 4 5 6 /6 GO Lecture 17 Reactor Theory-II Cylindrical Reactor The boundary conditions are: As Y 0 blows up at r = 0, hence A2 = 0 Thus the solution reduces to Now applying the vanishing flux boundary condition, we get Thus A1 = 0, which leads to the trivial solution. For non-trivial fundamental solution, or Thus the fundamental solution is 1 2 3 4 5 6 /6 GO Lecture 17 Reactor Theory-II A1 shall be similarly derived as done previously by using power. Consider a reactor that is producing power per unit length as P'. Consider a strip of thickness dr at a distance r from origin as shown. The volume of the strip is 2πrdrL, where L is the length of the reactor. Now we shall evaluate A1 as follows: No. of fissions per second = Energy released per second = Total Power, P = From tables J1(2.405) = 0.518. Thus, the flux distribution is given by As seen previously the power density will be maximum at the centre. Hence orificing has to be resorted to. We shall define the average flux such that power is conserved. Since peak flux = A1 More peaked than for slab reactor. 1 2 3 4 5 6 /6 GO
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