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

---
 1073/CH3/EX3.40/3_40.sce | 34 ++++++++++++++++++++++++++++++++++
 1 file changed, 34 insertions(+)
 create mode 100755 1073/CH3/EX3.40/3_40.sce

(limited to '1073/CH3/EX3.40')

diff --git a/1073/CH3/EX3.40/3_40.sce b/1073/CH3/EX3.40/3_40.sce
new file mode 100755
index 000000000..81064552e
--- /dev/null
+++ b/1073/CH3/EX3.40/3_40.sce
@@ -0,0 +1,34 @@
+
+clc;
+clear;
+//Exampe 3.40
+v=17.95*10^-6   //[m^2/s]
+dT=353-293  //[K]
+k=0.0283    //[W/m.K]
+g=9.81  //[m/s^2]
+Npr=0.698   //Prandtl number
+Cp=1005 //J/(kg.K)
+Tf=323  //Film temperature in [K]
+Beta=1/Tf   //[K^-1]
+l=1 //[m]
+Nra=(g*Beta*dT*(l^3)*Npr)/(v^2)
+
+//In textbook result of above statement is wrongly calculated,So
+Nra=3.95*10^8
+//For Nra <10^9,for a vertical plate,the average nusselt number is
+Nnu=0.59*Nra^(1.0/4.0)  //Nusselt number
+h=Nnu*k/l   //[W/m^2.K]
+h=2.35      //Approx in book
+A=l^2   //Area [m^2]
+//Heat loss form 4 vertical faces of 1m*1m is 
+Q1=4*(h*A*dT)   //[W]
+//For top surface 
+P=4*l   //Perimeter in [m]
+L=A/P   //[m]
+Nra=(Npr*g*Beta*dT*(L^3))/(v^2)
+Nnu=0.15*Nra^(1.0/3.0)  //Nusselt number
+h=Nnu*k/L   //[W/m^2.K]
+h=6.7           //Approx
+Q2=h*A*dT   //[W]
+Q_total=Q1+Q2   //Total heat loss[W]
+printf("\n Therefore total heat loss is %d W",Q_total);
-- 
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