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authorpriyanka2015-06-24 15:03:17 +0530
committerpriyanka2015-06-24 15:03:17 +0530
commitb1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch)
treeab291cffc65280e58ac82470ba63fbcca7805165 /1484/CH8
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initial commit / add all books
Diffstat (limited to '1484/CH8')
-rwxr-xr-x1484/CH8/EX8.1/8_1.sce12
-rwxr-xr-x1484/CH8/EX8.10/8_10.sce15
-rwxr-xr-x1484/CH8/EX8.11/8_11.sce14
-rwxr-xr-x1484/CH8/EX8.12/8_12.sce7
-rwxr-xr-x1484/CH8/EX8.2/8_2.sce13
-rwxr-xr-x1484/CH8/EX8.3/8_3.sce15
-rwxr-xr-x1484/CH8/EX8.4/8_4.sce14
-rwxr-xr-x1484/CH8/EX8.5/8_5.sce12
-rwxr-xr-x1484/CH8/EX8.6/8_6.sce14
-rwxr-xr-x1484/CH8/EX8.7/8_7.sce20
-rwxr-xr-x1484/CH8/EX8.8/8_8.sce21
-rwxr-xr-x1484/CH8/EX8.9/8_9.sce15
12 files changed, 172 insertions, 0 deletions
diff --git a/1484/CH8/EX8.1/8_1.sce b/1484/CH8/EX8.1/8_1.sce
new file mode 100755
index 000000000..8107fc37d
--- /dev/null
+++ b/1484/CH8/EX8.1/8_1.sce
@@ -0,0 +1,12 @@
+
+clc
+//initialisation of variables
+d= 1 //in
+v= 36 //ft/sec
+a= 30 //degrees
+w= 62.4 //lbs/ft^3
+g=32.2
+//CALCULATIONS
+P= w*sind(a)*v^2*(%pi*(d/12)^2/4)/g
+//RESULTS
+printf ('Total thrust on the plate= %.2f lb wt',P)
diff --git a/1484/CH8/EX8.10/8_10.sce b/1484/CH8/EX8.10/8_10.sce
new file mode 100755
index 000000000..8387160b8
--- /dev/null
+++ b/1484/CH8/EX8.10/8_10.sce
@@ -0,0 +1,15 @@
+clc
+//initialisation of variables
+vr= 20 //f/sec
+u= 9 //knots
+D= 64 //lbs per cubic foot
+g= 32.2 //ft/sec^2
+p= 40 //per cent
+//CALCULATIONS
+u1= u*6080/3600
+v= vr-u1
+P= D*2*vr*4.8/g
+HP= P*u1/550
+HP1= 100*HP/p
+//RESULTS
+printf ('cylinder H.P= %.2f H.P',HP1)
diff --git a/1484/CH8/EX8.11/8_11.sce b/1484/CH8/EX8.11/8_11.sce
new file mode 100755
index 000000000..c0192c984
--- /dev/null
+++ b/1484/CH8/EX8.11/8_11.sce
@@ -0,0 +1,14 @@
+clc
+//initialisation of variables
+W= 62.4 //lbs/ft^3
+A= 4 //ft^2
+P= 1000 //lbs
+g= 32.2 //ft/sec^2
+v= 10 //ft/sec
+//CALCULATIONS
+vr= sqrt(25+(P*g/(W*A)))+5
+Q= vr*W*A/10
+e= 2*v*100/(vr+v)
+//RESULTS
+printf ('quantity of water pumped= %.1f lbs',Q)
+printf ('\n efficiency= %.1f per cent',e)
diff --git a/1484/CH8/EX8.12/8_12.sce b/1484/CH8/EX8.12/8_12.sce
new file mode 100755
index 000000000..760d81191
--- /dev/null
+++ b/1484/CH8/EX8.12/8_12.sce
@@ -0,0 +1,7 @@
+clc
+//initialisation of variables
+g= 32.2 //ft/sec^2
+//CALCULATIONS
+v= sqrt(32*g)
+//RESULTS
+printf ('speed that delivery commence= %.1f ft/sec',v)
diff --git a/1484/CH8/EX8.2/8_2.sce b/1484/CH8/EX8.2/8_2.sce
new file mode 100755
index 000000000..fd12fa643
--- /dev/null
+++ b/1484/CH8/EX8.2/8_2.sce
@@ -0,0 +1,13 @@
+clc
+//initialisation of variables
+a= 180 //degrees
+g= 32.2 //ft/sec^2
+w= 62.4 //lbs/ft^3
+d= 1 //in
+H= 100 //ft
+u= 0.95
+//CALCULATIONS
+v= u*sqrt(2*g*H)
+Px= w*(1-cosd(a))*(%pi*(d/12)^2/4)*v^2/g
+//RESULTS
+printf ('force it exerts= %.1f lb wt',Px)
diff --git a/1484/CH8/EX8.3/8_3.sce b/1484/CH8/EX8.3/8_3.sce
new file mode 100755
index 000000000..7f0c25b7d
--- /dev/null
+++ b/1484/CH8/EX8.3/8_3.sce
@@ -0,0 +1,15 @@
+
+clc
+//initialisation of variables
+d= 30 //in
+a= 90 //degrees
+Q= 62.5 //ft^3/sec
+w= 62.4 //lbs/ft^3
+n=4
+g=32.2
+//CALCULATIONS
+v= Q*4/(%pi*(d/12)^2)
+P= w*%pi*(d/12)^2*v^2/(4*g)
+Px= P/n
+//RESULTS
+printf ('pull on each bolt= %.1f lbs',Px)
diff --git a/1484/CH8/EX8.4/8_4.sce b/1484/CH8/EX8.4/8_4.sce
new file mode 100755
index 000000000..a335ab8be
--- /dev/null
+++ b/1484/CH8/EX8.4/8_4.sce
@@ -0,0 +1,14 @@
+clc
+//initialisation of variables
+d= 4 //in
+v= 30 //ft/sec
+a= 22.5 //degrees
+w= 62.4 //lbs/ft^3
+g= 32.2 //ft/sec^2
+//CALCULATIONS
+P= w*(%pi*(d/12)^2/4)*v^2*sqrt(2*(1-cosd(a)))/g
+//RESULTS
+printf ('Resultant force tending to move the pipe= %.f lbs',P)
+
+
+//ANSWER GIVEN IN THE TEXTBOOK IS WRONG
diff --git a/1484/CH8/EX8.5/8_5.sce b/1484/CH8/EX8.5/8_5.sce
new file mode 100755
index 000000000..7a2923db0
--- /dev/null
+++ b/1484/CH8/EX8.5/8_5.sce
@@ -0,0 +1,12 @@
+clc
+//initialisation of variables
+d= 3 //in
+v1= 80 //ft/sec
+v2= 40 //ft/sec
+w= 62.4 //lbs/ft^3
+g= 32.2 //ft/sec^2
+//CALCULATIONS
+vr= v1-v2
+P= w*vr*v2*%pi*(d/12)^2/(g*4)
+//RESULTS
+printf ('normal pressure on the plate when jet strikes= %.1f lbs',P)
diff --git a/1484/CH8/EX8.6/8_6.sce b/1484/CH8/EX8.6/8_6.sce
new file mode 100755
index 000000000..8bcc89eed
--- /dev/null
+++ b/1484/CH8/EX8.6/8_6.sce
@@ -0,0 +1,14 @@
+clc
+//initialisation of variables
+d= 2 //in
+v1= 50 //ft/sec
+v2= 20 //ft/sec
+W= 62.4 //lbs/ft^3
+g= 32.2 //ft/sec^2
+//CALCULATIONS
+vr= v1-v2
+P= W*vr*v1*%pi*(d/2)^2/(g*4)
+W= P*v2
+KE= 2*vr*v2*100/v1^2
+//RESULTS
+printf ('Efficiency= %.f per cent',KE)
diff --git a/1484/CH8/EX8.7/8_7.sce b/1484/CH8/EX8.7/8_7.sce
new file mode 100755
index 000000000..a0506be38
--- /dev/null
+++ b/1484/CH8/EX8.7/8_7.sce
@@ -0,0 +1,20 @@
+clc
+//initialisation of variables
+d= 1 //in
+v= 10 //f/sec
+v1= 30 //ft/sec
+w= 62.4 //lbs/ft^3
+a= 180 //degrees
+g= 32.2 //ft/sec^2
+//CALCULATIONS
+A= %pi*(d/12)^2/4
+vr= 80-v1
+M= w*vr*A
+Px= M*vr*(1-cosd(a))/g
+W= Px*v1
+M1= w*80*A
+Px1= M1*vr*(1-cosd(a))/g
+W1= Px1*v1
+//RESULTS
+printf ('total force when there is a single cup= %.1f ft lbs',W)
+printf ('\n total force when there is a series of cups= %.1f ft lbs',W1)
diff --git a/1484/CH8/EX8.8/8_8.sce b/1484/CH8/EX8.8/8_8.sce
new file mode 100755
index 000000000..90ea002a6
--- /dev/null
+++ b/1484/CH8/EX8.8/8_8.sce
@@ -0,0 +1,21 @@
+clc
+//initialisation of variables
+v= 100 //ft/sec
+u= 40 //ft/sec
+a= 25 //degrees
+g= 32.2 //ft/sec^2
+vr= 66 //ft/sec
+a1= 20 ///degrees
+a2= 8 //degrees
+r= 0.14
+//CALCULATIONS
+A= atand(v*sind(a)/(v*cosd(a)-u))
+A1= atand(r)
+v1= vr*sind(A1)/sind(a1)
+W= (v^2-v1^2)/(2*g)
+e= (v^2-v1^2)*100/v^2
+//RESULTS
+printf ('inlet blade angle = %.2f degrees',A)
+printf ('\n outlet blade angle = %.2f degrees',A1)
+printf ('\n Work done = %.f ft lbs',W)
+printf ('\n efficiency = %.2f ft per cent',e)
diff --git a/1484/CH8/EX8.9/8_9.sce b/1484/CH8/EX8.9/8_9.sce
new file mode 100755
index 000000000..959b8673f
--- /dev/null
+++ b/1484/CH8/EX8.9/8_9.sce
@@ -0,0 +1,15 @@
+clc
+//initialisation of variables
+Q= 60 //ft^3/sec
+v= 12 //m.p.h
+A= 3 //ft^2
+D= 64 //lbs/ft^3
+g= 32.2 //ft/sec^2
+M= 64 //lbs
+//CALCULATIONS
+vr= Q/A
+u= v*44/30
+v1= vr-u
+P= M*Q*v1/g
+//RESULTS
+printf ('propelling force= %.1f lbs',P)