From b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b Mon Sep 17 00:00:00 2001 From: priyanka Date: Wed, 24 Jun 2015 15:03:17 +0530 Subject: initial commit / add all books --- 405/CH8/EX8.10/8_10.sce | 40 ++++++++++++++++++++++++++++++++++++++++ 1 file changed, 40 insertions(+) create mode 100755 405/CH8/EX8.10/8_10.sce (limited to '405/CH8/EX8.10/8_10.sce') diff --git a/405/CH8/EX8.10/8_10.sce b/405/CH8/EX8.10/8_10.sce new file mode 100755 index 000000000..eacacf30f --- /dev/null +++ b/405/CH8/EX8.10/8_10.sce @@ -0,0 +1,40 @@ +clear; +clc; +printf("\t\t\tExample Number 8.10\n\n\n"); +// heat transfer reduction with parallel plate shield +// Example 8.10 (page no.-413) +// solution + +E1 = 0.3;// emissivity of first plane +E2 = 0.8;// emissivity of second plane +E3 = 0.04;// emissivity of shield +sigma = 5.669*10^(-8);// [W/square meter K^(4)] +// the heat transfer without the shield is given by +// q_by_A = sigma*(T1^4-T2^4)/((1/E1)+(1/E2)-1) = 0.279*sigma*(T1^4-T2^4) +// where T1 is temperature of first plane and T2 is temperature of second plane +// the radiation network for the problem with the shield in place is shown in figure (8-32) (page no.-410). +// the resistances are +R1 = (1-E1)/E1; +R2 = (1-E2)/E2; +R3 = (1-E3)/E3; +// the total resistance with the shield is +R = R1+R2+R3; +// and the heat transfer is +// q_by_A = sigma*(T1^4-T2^4)/R = 0.01902*sigma*(T1^4-T2^4) +printf("so the heat tranfer is reduced by %f percent",((0.279-0.01902)/0.279)*100); + + + + + + + + + + + + + + + + -- cgit