Омские Новости
June 16th, 2019
3.1. Direct integration for a differential element to a circular disk on a plane parallel to that of the element
Let us consider the proposed figure. In order to determine the radiant interchange between an emitting circle, which lies in the plane ZX, and a point P situated in another parallel plane XY, the following coordinate system is proposed (Figure 2).
Terms depicted in figure 2 are:
d: vertical distance between the center of the emitting circle and the plane XY.
b: horizontal distance between differential element dAj and the plane ZX that contains the said circle.
r: Emitting surface radius.
S: Distance between differential elements (in the canonical equation (1) of the configuration factor, it is denoted as r, but in order to differentiate it from radius of the disk (emitting surface, r), we shift to this denomination).
According to figure 2, the differential element dA2 is expressed in terms of r and 0. Thus, to receive a proper integral, the rest of elements inside the integration sign of the canonical equation (1) should be expressed using the said variables. Basic construction for this expression
can be found in numerous manuals of radiative transfer [4]. Furthermore, mathematical support for the integration process is described in references [5]
dA1 represents the point source
dA2 = rdrdO
cosq
S = r2 + d2 + b2 – 2dr cosq
Substituting terms from (2) in accordance to figure 2, in the canonical equation of radiative transfer (1), the main integral that we need to solve is,
Operating in the numerator we can decompose this integral in two parts:
The limits for inner and outer integral are, respectively: from 0 to 2n, and from 0 to a, that is, the whole extension of the radius of the emitting circle.
In order to solve this double integral, we first integrate with respect to 0. Proceeding with the first integral implies taking out all the constants that are independent of 0, and this yields:
Such expression corresponds to a type, which yields the solution:
The change of variables is defined thus:
de = dx B = r2 + d2 + b2 C = 2dr A = 1 (10)
Before operating, and in order to simplify the otherwise tedious calculations, this expression can be put in simpler form by applying logical deductions. Focusing our attention in the first term of (9):
Csin( Ax)
A(B2 – C2) (B + Ccos(Ax)) (11)
It can be observed that sin(Ax) is in the numerator; if A=1 the former means that we have sin(X); but we need to bear in mind that the limits for our defined integral are 2n and 0, thus, sin(2n), sin(0), equal nil and so does the integral,
Subsequently, we focus our attention in the second term of equation (9);
So far, we have solved all terms outside the integration sign of equation (9). What remains inside the integral admits this change:
Therefore, substituting all terms we receive:
Once more, some logics were employed in order to compact the calculations; concentrating on the third term of (15), we find an the arctangent and a tangent expression. Bearing in mind that the limits of integration are (2n, 0), the result of arctangent is obviously n, and that produces:
The value of n is taken out of the integration mark and eliminated by means of the canonical equation of the configuration factor. That yields:
Again making some arrangements to these elements to produce an expression that enables easy integration, let us multiply the numerator and denominator by 4 and add and subtract a new term, 2rd2, always bearing in mind to reproduce the original expression in (17); that gives the following equation.
a 4 (r(r2 + d2 + b2) – 2rd2 + 2rd2)
2b2 J 3 ■■ dr
0 4 ((r2 + d2 + b2 )2 – 4d V J2
Decomposing and operating again:















a
2b 2d2 f————
0 (t1 + lp(b2
dt
d2) + (b2 + d2)2 f2
This integral responds to the following model with the solution:
Making the substitution:
Finally, adding both terms, from (21) and (27), in order to obtain the final result: b2 b2 a2 + b2 – d2 b2 – d2
2^1 ((a2 + d2 + b2)2 – 4d2a2)
2.2. Direct integration for a differential element to a circular disk on a plane perpendicular to that of element
In the perpendicular plane, that is, the ZX plane, according to the defined coordinate reference system, the main equation to be solved is:
This can be decomposed into two terms
The first part of this expression has already been solved, but with b2 instead of b d as a constant. The first term was solved in two parts, which were expressed in equations (21) and (27). From equation (21):
a
Now, equation (27) is rearranged as follows:














Next, assemble equations (31) and (32), group terms by common denominator and operate:




d (a2 + b2 – d2) 2b2d 2b2d – d {b2 – d2)
2b J((a2 + d2 + b2)2 – 4d2a2) 2b(d2 + b’)
a2d – b2d – d3 b2d + d3
2bJ((a2 + d2 + b2)2 – 4d2a2) 2b(d2 + b’)











Also, the second term from equations (30):
Finally, in order to produce the final solution for the perpendicular plane, it is required to assemble equations (33) and (39). Grouping and rearranging by common denominators it yields:




b2(a2 + b2 + d2)________ b_
2bdyj(a2 + b2 + d2)2 4d2a2 2bd
Again, this result can be checked against usual formulas that appear in numerous configuration factor catalogues, although those do not completely solve the problem. Only they work when the element is in a plane that passes through the center of the circle. A more general solution of a vector nature had been presented by the authors in other texts [6],[7]. In this chapter a sound relationship between the two fundamentals expressions has been found.
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