From 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 Mon Sep 17 00:00:00 2001
From: prashantsinalkar
Date: Tue, 10 Oct 2017 12:27:19 +0530
Subject: initial commit / add all books

---
 629/CH4/EX4.12/ex4_12.txt      |  5 +++++
 629/CH4/EX4.12/example4_12.sce | 14 ++++++++++++++
 629/CH4/EX4.13/ex4_13.txt      |  2 ++
 629/CH4/EX4.13/example4_13.sce | 11 +++++++++++
 629/CH4/EX4.2/ex4_2.txt        |  2 ++
 629/CH4/EX4.2/example4_2.sce   | 12 ++++++++++++
 629/CH4/EX4.3/ex4_3.txt        |  4 ++++
 629/CH4/EX4.3/example4_3.sce   | 17 +++++++++++++++++
 629/CH4/EX4.4/ex4_4.txt        |  3 +++
 629/CH4/EX4.4/example4_4.sce   | 12 ++++++++++++
 629/CH4/EX4.5/ex4_5.txt        |  2 ++
 629/CH4/EX4.5/example4_5.sce   | 19 +++++++++++++++++++
 629/CH4/EX4.6/ex4_6.txt        |  2 ++
 629/CH4/EX4.6/example4_6.sce   | 10 ++++++++++
 629/CH4/EX4.7/ex4_7.txt        |  3 +++
 629/CH4/EX4.7/example4_7.sce   |  9 +++++++++
 629/CH4/EX4.8/ex4_8.txt        |  3 +++
 629/CH4/EX4.8/example4_8.sce   | 17 +++++++++++++++++
 629/CH4/EX4.9/ex4_9.txt        |  3 +++
 629/CH4/EX4.9/example4_9.sce   | 11 +++++++++++
 20 files changed, 161 insertions(+)
 create mode 100644 629/CH4/EX4.12/ex4_12.txt
 create mode 100644 629/CH4/EX4.12/example4_12.sce
 create mode 100644 629/CH4/EX4.13/ex4_13.txt
 create mode 100644 629/CH4/EX4.13/example4_13.sce
 create mode 100644 629/CH4/EX4.2/ex4_2.txt
 create mode 100644 629/CH4/EX4.2/example4_2.sce
 create mode 100644 629/CH4/EX4.3/ex4_3.txt
 create mode 100644 629/CH4/EX4.3/example4_3.sce
 create mode 100644 629/CH4/EX4.4/ex4_4.txt
 create mode 100644 629/CH4/EX4.4/example4_4.sce
 create mode 100644 629/CH4/EX4.5/ex4_5.txt
 create mode 100644 629/CH4/EX4.5/example4_5.sce
 create mode 100644 629/CH4/EX4.6/ex4_6.txt
 create mode 100644 629/CH4/EX4.6/example4_6.sce
 create mode 100644 629/CH4/EX4.7/ex4_7.txt
 create mode 100644 629/CH4/EX4.7/example4_7.sce
 create mode 100644 629/CH4/EX4.8/ex4_8.txt
 create mode 100644 629/CH4/EX4.8/example4_8.sce
 create mode 100644 629/CH4/EX4.9/ex4_9.txt
 create mode 100644 629/CH4/EX4.9/example4_9.sce

(limited to '629/CH4')

diff --git a/629/CH4/EX4.12/ex4_12.txt b/629/CH4/EX4.12/ex4_12.txt
new file mode 100644
index 000000000..b067ae916
--- /dev/null
+++ b/629/CH4/EX4.12/ex4_12.txt
@@ -0,0 +1,5 @@
+ 
+The velocity at 10km from the center = 16 m/s.
+
+The pressure difference between two locations = 806 Pa.
+ 
\ No newline at end of file
diff --git a/629/CH4/EX4.12/example4_12.sce b/629/CH4/EX4.12/example4_12.sce
new file mode 100644
index 000000000..7639c1e58
--- /dev/null
+++ b/629/CH4/EX4.12/example4_12.sce
@@ -0,0 +1,14 @@
+clear
+clc
+//Example 4.12 VELOCITY AND PRESSURE DISTRIBUTION IN A FREE VORTEX
+rho=1.2; //density[kg/m^3]
+r1=4; //[km]
+r2=10; //[km]
+V1=40; //velocity[m/s]
+//Velocity distribution, V=C/r
+C=r1*V1 
+V2=C/r2 //[m/s]
+printf("\nThe velocity at 10km from the center = %.f m/s.\n",V2)
+//Bernoulli equation, for horizontal plane
+delp=rho*(V1^2-V2^2)/2 //delp=p2-p1,[Pa]
+printf("\nThe pressure difference between two locations = %.f Pa.\n",delp)
\ No newline at end of file
diff --git a/629/CH4/EX4.13/ex4_13.txt b/629/CH4/EX4.13/ex4_13.txt
new file mode 100644
index 000000000..59d095eeb
--- /dev/null
+++ b/629/CH4/EX4.13/ex4_13.txt
@@ -0,0 +1,2 @@
+ 
+The pressure difference between center and outer edge of mercury = -1.59 in Hg
\ No newline at end of file
diff --git a/629/CH4/EX4.13/example4_13.sce b/629/CH4/EX4.13/example4_13.sce
new file mode 100644
index 000000000..41b34a273
--- /dev/null
+++ b/629/CH4/EX4.13/example4_13.sce
@@ -0,0 +1,11 @@
+clear
+clc
+//Example 4.13 PRESSURE DIFFERENCE IN TORNADO
+//1mi=5280ft, 1hr=3600s
+V=150*5280/3600 //[ft/s]
+//1slug=32.2lbm
+rho=0.075/32.2 //density[slug/ft^3]
+//Pressure difference, p1-p0=-rho*V^2
+//29.92 in Hg=2116 psf
+delp=-rho*V^2*(29.92/2116) //inches of Hg
+printf("\nThe pressure difference between center and outer edge of mercury = %.2f in Hg.\n",delp)
\ No newline at end of file
diff --git a/629/CH4/EX4.2/ex4_2.txt b/629/CH4/EX4.2/ex4_2.txt
new file mode 100644
index 000000000..f82815e54
--- /dev/null
+++ b/629/CH4/EX4.2/ex4_2.txt
@@ -0,0 +1,2 @@
+ 
+The gage pressure on the piston, p = 11.0 kPa, gage.
\ No newline at end of file
diff --git a/629/CH4/EX4.2/example4_2.sce b/629/CH4/EX4.2/example4_2.sce
new file mode 100644
index 000000000..d53b32650
--- /dev/null
+++ b/629/CH4/EX4.2/example4_2.sce
@@ -0,0 +1,12 @@
+clear
+clc
+//Example 4.2 APPLICATION OF EULER’S EQUATION TO ACCELERATION OF A FLUID
+g=9.81; //[m/s^2]
+az=100; //acceleration in z direction [m/s^2]
+rho=10^3; //[kg/m^3]
+//Integrating, d(p+g*rho*z)/dz=-rho*az
+//(p2+rho*g*z2)-(p1+rho*g*z1)=-rho*az*(z2-z1)
+delz=0.1; //delz=z2-z1,[m]
+p2=0;
+p1=(p2+rho*(g+az)*delz)/10^3 //[kPa]
+printf("\nThe gage pressure on the piston, p = %.1f kPa, gage.\n",p1)
\ No newline at end of file
diff --git a/629/CH4/EX4.3/ex4_3.txt b/629/CH4/EX4.3/ex4_3.txt
new file mode 100644
index 000000000..8e3d17ada
--- /dev/null
+++ b/629/CH4/EX4.3/ex4_3.txt
@@ -0,0 +1,4 @@
+ 
+(a)The pressure at the top front, p = 261 psfg (= 12.5 kPa,gage).
+
+(b)The maximum pressure in the tank, pmax = 513 psfg (= 24.6 kPa,gage)
\ No newline at end of file
diff --git a/629/CH4/EX4.3/example4_3.sce b/629/CH4/EX4.3/example4_3.sce
new file mode 100644
index 000000000..783c2a930
--- /dev/null
+++ b/629/CH4/EX4.3/example4_3.sce
@@ -0,0 +1,17 @@
+clear
+clc
+//Example 4.3 PRESSURE IN A DECELERATING TANK OF LIQUID
+p1=0;
+Gamma=42; //[lbf/ft^3]
+g=32.2; //[ft/s^2]
+al=-10; //[ft/s^2]
+l=20; //[ft]
+//Euler's equation along the top of tank, dp/dl=-Gamma*l/g
+p2=p1-Gamma*al*l/g //[psfg]
+//1kPa=20.88psfg
+printf("\n(a)The pressure at the top front, p = %.f psfg (= %.1f kPa,gage).\n",p2,p2/20.88)
+//Eulers equation in vertical direction,
+//d(p+Gamma*z)/dz=-rho*az, az=0
+delz=6; //delz=z2-z3,[ft]
+p3=p2+Gamma*delz //[psfg]
+printf("\n(b)The maximum pressure in the tank, pmax = %.f psfg (= %.1f kPa,gage).\n",p3,p3/20.88)
\ No newline at end of file
diff --git a/629/CH4/EX4.4/ex4_4.txt b/629/CH4/EX4.4/ex4_4.txt
new file mode 100644
index 000000000..b63c1ade1
--- /dev/null
+++ b/629/CH4/EX4.4/ex4_4.txt
@@ -0,0 +1,3 @@
+ 
+The elevation difference between the liquid at the center and the wall, during rotation = 0.051 m.
+ 
\ No newline at end of file
diff --git a/629/CH4/EX4.4/example4_4.sce b/629/CH4/EX4.4/example4_4.sce
new file mode 100644
index 000000000..2feeece3d
--- /dev/null
+++ b/629/CH4/EX4.4/example4_4.sce
@@ -0,0 +1,12 @@
+clear
+clc
+//Example 4.4 SURFACE PROFILE OF ROTATING LIQUID
+g=9.81; //[m/s^2]
+d=0.5; //[m]
+w=4; //(rad/s)
+//(p1/gamma)+z1-(w^2*r1^2/(2*g))=(p2/gamma)+z2-(w^2*r2^2/(2*g))
+//p1=p2
+r1=0; //[m]
+r2=d/2; //[m]
+delz=(w^2*(r2^2-r1^2)/(2*g)) //delz=(z2-z1),[m]
+printf("\nThe elevation difference between the liquid at the center and the wall, during rotation = %.3f m.\n",delz)
\ No newline at end of file
diff --git a/629/CH4/EX4.5/ex4_5.txt b/629/CH4/EX4.5/ex4_5.txt
new file mode 100644
index 000000000..45d806291
--- /dev/null
+++ b/629/CH4/EX4.5/ex4_5.txt
@@ -0,0 +1,2 @@
+ 
+The new levels of water in the tube are z1 = 0.021 m, z2 = 0.339 m.
\ No newline at end of file
diff --git a/629/CH4/EX4.5/example4_5.sce b/629/CH4/EX4.5/example4_5.sce
new file mode 100644
index 000000000..dabd3d8a8
--- /dev/null
+++ b/629/CH4/EX4.5/example4_5.sce
@@ -0,0 +1,19 @@
+clear
+clc
+//Example 4.5 ROTATING MANOMETER TUBE
+g=9.81; //[m/s^2]
+r1=0.18; //[m]
+r2=0.36; //[m]
+//Initial water levels
+h1=0.18; //[m]
+h2=0.18; //[m]
+w=8; //angular speed[rad/s]
+//-z1+z2=w^2*(r2^2-r1^2)/(2*g)
+//z1+z2=h1+h2
+A=[-1 1;1 1];
+B=[w^2*(r2^2-r1^2)/(2*g); h1+h2]
+//Az=B, z=(A^-1)*B, z=[z1;z2]
+z=inv(A)*B
+z1=z(1) //[m]
+z2=z(2) //[m]
+printf("\nThe new levels of water in the tube are z1 = %.3f m, z2 = %.3f m.\n",z1,z2)
\ No newline at end of file
diff --git a/629/CH4/EX4.6/ex4_6.txt b/629/CH4/EX4.6/ex4_6.txt
new file mode 100644
index 000000000..829524b52
--- /dev/null
+++ b/629/CH4/EX4.6/ex4_6.txt
@@ -0,0 +1,2 @@
+ 
+The velocity in the throat section = 3.62 m/s.
\ No newline at end of file
diff --git a/629/CH4/EX4.6/example4_6.sce b/629/CH4/EX4.6/example4_6.sce
new file mode 100644
index 000000000..4c542a50c
--- /dev/null
+++ b/629/CH4/EX4.6/example4_6.sce
@@ -0,0 +1,10 @@
+clear
+clc
+//Example 4.6 VELOCITY IN A VENTURI SECTION
+h1=1; //[m]
+h2=0.5; //[m]
+g=9.81; //[m/s^2]
+//h1-h2=(V2^2-V1^2)/(2*g), V2=2*V1
+V1=sqrt(2*g*(h1-h2)/3) //[m/s]
+V2=2*V1 //[m/s]
+printf("\nThe velocity in the throat section = %.2f m/s.\n",V2)
\ No newline at end of file
diff --git a/629/CH4/EX4.7/ex4_7.txt b/629/CH4/EX4.7/ex4_7.txt
new file mode 100644
index 000000000..74c3803cd
--- /dev/null
+++ b/629/CH4/EX4.7/ex4_7.txt
@@ -0,0 +1,3 @@
+ 
+The velocity of the liquid in the drain port = 14 m/s.
+ 
\ No newline at end of file
diff --git a/629/CH4/EX4.7/example4_7.sce b/629/CH4/EX4.7/example4_7.sce
new file mode 100644
index 000000000..348b16f21
--- /dev/null
+++ b/629/CH4/EX4.7/example4_7.sce
@@ -0,0 +1,9 @@
+clear
+clc
+//Example 4.7 OUTLET VELOCITY FROM DRAINING TANK
+g=9.81; //[m/s^2]
+delz=10; //delz=(z1-z2),[m]
+//(p1/gamma)+z1-(V1^2/(2*g))=(p2/gamma)+z2-(V2^2/(2*g)), p1=p2
+V1=0;//[m]
+V2=sqrt(V1^2+2*g*delz) //[m/s]
+printf("\nThe velocity of the liquid in the drain port = %.f m/s.\n",V2)
\ No newline at end of file
diff --git a/629/CH4/EX4.8/ex4_8.txt b/629/CH4/EX4.8/ex4_8.txt
new file mode 100644
index 000000000..77f02612c
--- /dev/null
+++ b/629/CH4/EX4.8/ex4_8.txt
@@ -0,0 +1,3 @@
+ 
+ The kerosene velocity in the pipe = 24.3 ft/s.
+ 
\ No newline at end of file
diff --git a/629/CH4/EX4.8/example4_8.sce b/629/CH4/EX4.8/example4_8.sce
new file mode 100644
index 000000000..0e7fd3ca6
--- /dev/null
+++ b/629/CH4/EX4.8/example4_8.sce
@@ -0,0 +1,17 @@
+clear
+clc
+//Example 4.8 APPLICATION OF PITOT EQUATION WITH MANOMETER
+g=32.2; //[ft/s^2]
+y=7/12; //[ft]
+//Specific gravities
+S_kero=0.81;
+S_Hg=13.55;
+//Specific weights
+g_water=62.4; //[lbf/ft^3]
+g_Hg=S_Hg*g_water //[lbf/ft^3]
+g_kero=S_kero*g_water //[lbf/ft^3]
+rho_kero=g_kero/g //density[lbm/ft^3]
+//Manometer equation, pz1-pz2=y*(gamma_Hg-gamma_kero)
+//Pitot-static tube equation, V=[2*(pz1-pz2)/rho]^(1/2)
+V=(2*y*(g_Hg-g_kero)/rho_kero)^(1/2) //[ft/s]
+printf("\n The kerosene velocity in the pipe = %.1f ft/s.\n",V)
\ No newline at end of file
diff --git a/629/CH4/EX4.9/ex4_9.txt b/629/CH4/EX4.9/ex4_9.txt
new file mode 100644
index 000000000..96318a86d
--- /dev/null
+++ b/629/CH4/EX4.9/ex4_9.txt
@@ -0,0 +1,3 @@
+ 
+The velocity of air in the tunnel = 35.4 m/s.
+ 
\ No newline at end of file
diff --git a/629/CH4/EX4.9/example4_9.sce b/629/CH4/EX4.9/example4_9.sce
new file mode 100644
index 000000000..cf0c9d0e5
--- /dev/null
+++ b/629/CH4/EX4.9/example4_9.sce
@@ -0,0 +1,11 @@
+clear
+clc
+//Example 4.9 PITOT TUBE APPLICATION WITH PRESSURE GAGE
+p=98*10^3; //pressure[N/m^3]
+R=287; //gas constant[J/kg.K]
+T=20+273; //temperature[K]
+rho=p/(R*T) //density[kg/m^3]
+del_p=730; //[N/m^2]
+//Pitot-static tube equation,
+V=sqrt(2*del_p/rho) //velocity[m/s]
+printf("\nThe velocity of air in the tunnel = %.1f m/s.\n",V)
\ No newline at end of file
-- 
cgit