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12th International Symposium on District Heating and Cooling

12th International Symposium on District Heating and Cooling

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The <str<strong>on</strong>g>12th</str<strong>on</strong>g> <str<strong>on</strong>g>Internati<strong>on</strong>al</str<strong>on</strong>g> <str<strong>on</strong>g>Symposium</str<strong>on</strong>g> <strong>on</strong> <strong>District</strong> <strong>Heating</strong> <strong>and</strong> <strong>Cooling</strong>,September 5 th to September 7 th , 2010, Tallinn, Est<strong>on</strong>iaMODELLING USING CONFORMAL COORDINATESIt is rather complicated to calculate the temperaturedecline in twin pipes due to the pipe geometry. A socalled c<strong>on</strong>formal mapping presented in [8] was used tomap the twin pipe geometry <strong>on</strong>to a rectangulargeometry. In the experimental measurements, thesupply <strong>and</strong> return service pipes were assumed to haveequal temperatures in the test-procedure. Then,symmetry is assumed between the four quarters of apipe cross-secti<strong>on</strong>. A quarter of a twin pipe is studied,see Fig. 5. In the x,y-plane, the temperaturedevelopment is described by the heat equati<strong>on</strong>:T T T c ( ( T) ) ( ( T) )t x x y y(1)The (x,y)-coordinates ( z x i y)are transformed tosuitable c<strong>on</strong>formal coordinates ( w u i v)with theaid of line sources <strong>and</strong> so called multipoles.water <strong>and</strong> the right-h<strong>and</strong> boundary against the pollwater. The heat flux in the vertical v-directi<strong>on</strong> is zero <strong>on</strong>the horiz<strong>on</strong>tal boundaries due to symmetry.Fig. 6 Initial temperature distributi<strong>on</strong> in the crosssecti<strong>on</strong>of a pipe quarter in the u, v-plane.In the numerical soluti<strong>on</strong>, the regi<strong>on</strong> is divided into arectangular mesh. The area factor is now the area ofeach of the cells shown in Fig.5. They are shown inFig. 7. The largest cell is the <strong>on</strong>e in the lower left cornerin Fig.5 near the stagnati<strong>on</strong> point (usp). The areas areused to calculate the heat capacity of each cell in the u-v-plane.Fig. 7 Areas of the computati<strong>on</strong>al cells in the x, y –planetransferred to a u, v-plane. The stagnati<strong>on</strong> point is denotedusp.Fig. 5 A quarter of a twin pipe in x-y-plane geometryThe heat equati<strong>on</strong> in the c<strong>on</strong>formal coordinates is:T T T c A( u, v) ( ( T) ) ( ( T) )t u u v vHere, A(u,v) is the area factor in the c<strong>on</strong>formaltransformati<strong>on</strong>.The c<strong>on</strong>sidered regi<strong>on</strong> shown in Fig. 5 is transformedto a rectangular regi<strong>on</strong> in the u, v-plane, see Fig. 6. Inthe figure, the left-h<strong>and</strong> boundary lies against the coil(2)The initial steady-state c<strong>on</strong>diti<strong>on</strong> for a twin pipe withcoil water temperature T w = 81.3ºC immersed into poolwater at T0=19.7ºC is showed in u-v coordinates inFigure 6. Then, the temperature decline of stagnantwater in the twin pipes are calculatedThe density ρ <strong>and</strong> the heat capacity c of thepolyurethane foam are assumed c<strong>on</strong>stant in thetemperature interval studied. The boundarytemperatures at the casing are given by the pooltemperature.The thermal c<strong>on</strong>ductivity λ(T) of the polyurethane foamis determined by the thermal c<strong>on</strong>ductivity at 50ºC λ 50(W/m·K) <strong>and</strong> a coefficient λ‟ to account for a lineartemperature dependence.50 50( T) 1 ' ( T T )(3)93

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