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

---
 530/CH3/EX3.14/example_3_14.sce | 33 +++++++++++++++++++++++++++++++++
 1 file changed, 33 insertions(+)
 create mode 100755 530/CH3/EX3.14/example_3_14.sce

(limited to '530/CH3/EX3.14/example_3_14.sce')

diff --git a/530/CH3/EX3.14/example_3_14.sce b/530/CH3/EX3.14/example_3_14.sce
new file mode 100755
index 000000000..96ed5ccdf
--- /dev/null
+++ b/530/CH3/EX3.14/example_3_14.sce
@@ -0,0 +1,33 @@
+clear;
+clc;
+
+// A Textbook on HEAT TRANSFER by S P SUKHATME
+// Chapter 3
+// Thermal Radiation
+
+// Example 3.14
+// Page 147
+printf("Example 3.14, Page 147 \n\n")
+
+D = 1 ; // [m]
+r = 6250 ; // [km]
+D_surf = 300 ; // [km]
+s = 5.670*10^-8;
+e = 0.3 ;
+Tc = -18+273 ; // [K]
+T_surf = 27+273 ; // [K]
+
+// Rate of emissino of radiant energy from the two faces of satellite disc
+r_emission = 2*e*%pi*((D/2)^2)*s*Tc^4; // [W]
+
+// A2*F21 = A1*F12
+sina = (r/(r+D_surf));
+F12 = sina^2;
+
+// Rate at which the satellite receives and absorbs energy coming from earth
+r_receive = e*s*(%pi*((D/2)^2))*F12*T_surf^4; // [W]
+
+r_loss = r_emission - r_receive; // [W]
+
+printf("Net Rate at which energy is leaving the satellite = %f W",r_loss);
+
-- 
cgit