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
---
1358/CH3/EX3.4/Example34.sce | 24 ++++++++++++++++++++++++
1 file changed, 24 insertions(+)
create mode 100755 1358/CH3/EX3.4/Example34.sce
(limited to '1358/CH3/EX3.4/Example34.sce')
diff --git a/1358/CH3/EX3.4/Example34.sce b/1358/CH3/EX3.4/Example34.sce
new file mode 100755
index 000000000..daf99599b
--- /dev/null
+++ b/1358/CH3/EX3.4/Example34.sce
@@ -0,0 +1,24 @@
+// Display mode
+mode(0);
+// Display warning for floating point exception
+ieee(1);
+clear;
+clc;
+disp("Turbomachinery Design and Theory,Rama S. R. Gorla and Aijaz A. Khan, Chapter 3, Example 4")
+disp("Given Data")
+H = 505//Head in m
+P = 12900//Power in kW
+N = 425//Speed in rpm
+etao = 0.84//Efficiency
+g = 9.81//m/s2
+disp("Let Q be the discharge of the turbine")
+Q = P/(etao*g*H)
+disp("Velocity of jet C")
+Cv = 0.98;
+C = Cv * (2*g*H)^0.5
+disp("Tangential velocity of the wheel is given by ")
+U = 0.46*C
+disp("Diameter D")
+D = 60*U/(%pi*N)
+disp("Let d be the diameter of the nozzle. The discharge through the nozzle must be equal to the discharge of the turbine. Therefore")
+d = (Q*4/(%pi*C))^0.5
--
cgit