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/EX3.14/Example314.sce | 23 +++++++++++++++++++++++
 1 file changed, 23 insertions(+)
 create mode 100755 1358/CH3/EX3.14/Example314.sce

(limited to '1358/CH3/EX3.14/Example314.sce')

diff --git a/1358/CH3/EX3.14/Example314.sce b/1358/CH3/EX3.14/Example314.sce
new file mode 100755
index 000000000..09b70d038
--- /dev/null
+++ b/1358/CH3/EX3.14/Example314.sce
@@ -0,0 +1,23 @@
+// 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 14")
+disp("Discharge, Q")
+Q = 0.5//m3/s
+disp("Velocity of flow at inlet, Cr1")
+Cr1 = 1.5//m/s
+disp("Velocity of periphery at inlet, U1")
+U1 = 20
+disp("Velocity of whirl at inlet, Cw1")
+Cw1 = 15
+disp("As the velocity of flow is constant, Cr1 = Cr2")
+Cr2 = Cr1
+disp("Let beta1 = vane angle at inlet")
+disp("From inlet velocity triangle")
+beta1 = 180 - atan(Cr1/(U1-Cw1)) *180/%pi
+g = 9.81;
+disp("Since the discharge is radial at outlet, and so the velocity of whirl at outlet is zero. Therefore,")
+H = Cw1*U1/g + Cr1^2/(2*g)//m
-- 
cgit