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1 Indicates cells that require user input. 1 Indicates cells that give the output. Internal Temperature, T i o C External/Ambient Temperature, T o o C Heat transfer coefficient for heat transfer inside, α i kcal/m 2 h o C or W/m 2 K Heat transfer coefficient for heat transfer outside, α o kcal/m 2 h o C or W/m 2 K Total resistance at internal surface, R i m 2 h o C/kcal or m 2 K/W Total resistance at outer surface, R o m 2 h o C/kcal or m 2 K/W Temperature at 1st refractory layer surface, T h = T i - (q x R i ) o C Thickness, S mm Thermal conductivity, K kcal/mh o C or W/mK Thermal resistance, R n = S/(K x 1000) m 2 h o C/kcal or m 2 K/W Border layer Temperature, T n = T n-1 - (q x R n ) o C Temp drop across layer, T n+1 - T n o C Total Thermal resistance, R = R i +R 1 +R 2 +R 3 +R o m 2 h o C/kcal or m 2 K/W Heat flow (flux) density, q = (T i - T o ) / R kcal/m 2 h or W/m 2 o C o C o C o C o C o C o C Ti = T h = T 1 = T 2 = T 3 = T 4 = T o = 217 217 216 55 1000 217 948 217 216 0 1 Diagramic representation of Ouput 948 CALCULATION SHEET FOR TEMPERATURE DROP ACROSS REFRACTORY Description Unit 0.0003 Metal shell 80 0 0 8 1 731 1 0 217 0 0.287 0.2787 30.11 1st Refractory layer 2nd Refractory layer 3rd Refractory layer 0.3604 2622 0 1000 55 50 16.29 0.0200 0.0614 217

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  • 1 Indicates cells that require user input.

    1 Indicates cells that give the output.

    Internal Temperature, TioC

    External/Ambient Temperature, TooC

    Heat transfer coefficient for heat transfer inside, i kcal/m2h

    oC or W/m

    2K

    Heat transfer coefficient for heat transfer outside, o kcal/m2h

    oC or W/m

    2K

    Total resistance at internal surface, Ri m2h

    oC/kcal or m

    2K/W

    Total resistance at outer surface, Ro m2h

    oC/kcal or m

    2K/W

    Temperature at 1st refractory layer surface, Th = Ti - (q x Ri)oC

    Thickness, S mm

    Thermal conductivity, K kcal/mhoC or W/mK

    Thermal resistance, Rn = S/(K x 1000) m2h

    oC/kcal or m

    2K/W

    Border layer Temperature, Tn= Tn-1 - (q x Rn)oC

    Temp drop across layer, Tn+1 - TnoC

    Total Thermal resistance, R = Ri+R1+R2+R3+Ro m2h

    oC/kcal or m

    2K/W

    Heat flow (flux) density, q = (Ti - To) / R kcal/m2h or W/m

    2

    oC

    oC

    oC

    oC

    oC

    oC

    oC

    Ti =

    Th =

    T1 =

    T2 =

    T3 =

    T4 =

    To =

    217

    217

    216

    55

    1000

    217

    948

    217 216

    0 1

    Diagramic representation of Ouput

    948

    CALCULATION SHEET FOR TEMPERATURE DROP ACROSS REFRACTORY

    Description Unit

    0.0003

    Metal shell

    80 0 0 8

    1

    731

    1

    0

    217

    0

    0.287

    0.2787

    30.11

    1st Refractory

    layer

    2nd Refractory

    layer

    3rd Refractory

    layer

    0.3604

    2622

    0

    1000

    55

    50

    16.29

    0.0200

    0.0614

    217