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Original file line number | Diff line number | Diff line change |
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Geometry.CopyMeshingMethod = 1; | ||
R = 72.5; | ||
H = 2*R + 6.75; | ||
num_segments = 14; | ||
pitch = R / num_segments; | ||
x = .237952211; | ||
fuel_rad = x * pitch; | ||
graph_rad = pitch; | ||
lc = 1; | ||
lx = .4; | ||
ly = 10; | ||
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||
Point(1) = {0, 0, 0, lc}; | ||
Point(2) = {fuel_rad, 0, 0, lc}; | ||
Point(3) = {graph_rad, 0, 0, lc}; | ||
Point(4) = {0, H, 0, lc}; | ||
Point(5) = {fuel_rad, H, 0, lc}; | ||
Point(6) = {graph_rad, H, 0, lc}; | ||
// fuel top | ||
Line(1) = {4, 5}; | ||
// graph top | ||
Line(2) = {5, 6}; | ||
// graph right edge | ||
Line(3) = {6, 3}; | ||
// graph bottom | ||
Line(4) = {3, 2}; | ||
// fuel bottom | ||
Line(5) = {1, 2}; | ||
// fuel-graph interface | ||
Line(6) = {2, 5}; | ||
// fuel left edge | ||
Line(7) = {4, 1}; | ||
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// Fuel | ||
Line Loop(8) = {1, -6, -5, -7}; | ||
Plane Surface(9) = {8}; | ||
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// Moderator | ||
Line Loop(10) = {2, 3, 4, 6}; | ||
Plane Surface(11) = {10}; | ||
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// Structured | ||
Transfinite Line{1, 5} = fuel_rad/lx; | ||
Transfinite Line{2, 4} = (graph_rad - fuel_rad)/lx; | ||
Transfinite Line{3, 6, 7} = H/ly; | ||
Transfinite Surface{9}; | ||
Transfinite Surface{11}; | ||
Recombine Surface{9}; | ||
Recombine Surface{11}; | ||
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||
fuel_surfaces[] = {9}; | ||
moder_surfaces[] = {11}; | ||
fuel_tops[] = {1}; | ||
fuel_bottoms[] = {5}; | ||
moder_bottoms[] = {4}; | ||
moder_tops[] = {2}; | ||
For xindex In {1:num_segments-1} | ||
new_f_surface = Translate {xindex*pitch, 0, 0} { | ||
Duplicata { Surface{9}; } | ||
}; | ||
fuel_surfaces += new_f_surface; | ||
new_m_surface = Translate {xindex*pitch, 0, 0} { | ||
Duplicata { Surface{11}; } | ||
}; | ||
moder_surfaces += new_m_surface; | ||
fuel_tops += {13 + (xindex - 1) * 8}; | ||
moder_tops += {17 + (xindex - 1) * 8}; | ||
fuel_bottoms += {15 + (xindex - 1) * 8}; | ||
moder_bottoms += {19 + (xindex - 1) * 8}; | ||
EndFor // xindex | ||
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Physical Surface("fuel") = { fuel_surfaces[] }; | ||
Physical Surface("moder") = { moder_surfaces[] }; | ||
Physical Line("fuel_tops") = { fuel_tops[] }; | ||
Physical Line("moder_tops") = { moder_tops[] }; | ||
Physical Line("fuel_bottoms") = { fuel_bottoms[] }; | ||
Physical Line("moder_bottoms") = { moder_bottoms[] }; | ||
Physical Line("outer_wall") = { 18 + 8 * (num_segments - 2) }; |
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