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authorpriyanka2015-06-24 15:03:17 +0530
committerpriyanka2015-06-24 15:03:17 +0530
commitb1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch)
treeab291cffc65280e58ac82470ba63fbcca7805165 /2021/CH16
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Diffstat (limited to '2021/CH16')
-rwxr-xr-x2021/CH16/EX16.1/EX16_1.pdfbin0 -> 24880 bytes
-rwxr-xr-x2021/CH16/EX16.1/EX16_1.sce20
-rwxr-xr-x2021/CH16/EX16.3/EX16_3.pdfbin0 -> 15095 bytes
-rwxr-xr-x2021/CH16/EX16.3/EX16_3.sce11
-rwxr-xr-x2021/CH16/EX16.4/EX16_4.pdfbin0 -> 20263 bytes
-rwxr-xr-x2021/CH16/EX16.4/EX16_4.sce14
-rwxr-xr-x2021/CH16/EX16.5/EX16_5.pdfbin0 -> 20197 bytes
-rwxr-xr-x2021/CH16/EX16.5/EX16_5.sce11
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-rwxr-xr-x2021/CH16/EX16.6/EX16_6.sce42
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diff --git a/2021/CH16/EX16.1/EX16_1.pdf b/2021/CH16/EX16.1/EX16_1.pdf
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diff --git a/2021/CH16/EX16.1/EX16_1.sce b/2021/CH16/EX16.1/EX16_1.sce
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+//Finding of Lift,Drag,Power Required
+//Given
+A=4;
+V=40*(5/18);
+Cd1=0.8;
+Cd2=0.2;
+rho=1.25;
+//To Find
+FL=Cd1*A*rho*((V^2)/2);
+Fd=Cd2*A*rho*((V^2)/2);
+F=sqrt(FL^2+Fd^2);
+P=Fd*V;
+P1=P/1000;
+theta=(FL/Fd);
+theta1=(tan(theta))^-1;
+disp("Lift Force ="+string(FL)+" Newton");
+disp("Power Required ="+string(P1)+" Kilo Watts");
+disp("Drag Force ="+string(Fd)+" Newton");
+disp("Resultant Force ="+string(F)+" Newton");
+disp("Angle of Flow Direction ="+string(theta1)+" degrees");
diff --git a/2021/CH16/EX16.3/EX16_3.pdf b/2021/CH16/EX16.3/EX16_3.pdf
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diff --git a/2021/CH16/EX16.3/EX16_3.sce b/2021/CH16/EX16.3/EX16_3.sce
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+//Finding of Diameter
+//Given
+W=80*9.81;
+Fd=80*9.81;
+V=25;
+Cd=0.5;
+rho=1.25;
+//To Find
+D=(2*Fd)/(Cd*rho*(V^2)*(4/%pi));
+D1=sqrt(D);
+disp("Diameter ="+string(D1)+" meter");
diff --git a/2021/CH16/EX16.4/EX16_4.pdf b/2021/CH16/EX16.4/EX16_4.pdf
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diff --git a/2021/CH16/EX16.4/EX16_4.sce b/2021/CH16/EX16.4/EX16_4.sce
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+//Finding of Coefficient of Lift ,Drag
+//Given
+A=25;
+P=588.6*(7/10);
+FL=19620;
+V=200*(5/18);
+rho=1000;
+FD=7416;
+//To Find
+FD=(P*1000)/(V);
+Cd=(FD*2)/(rho*A*(V^2));
+Cl=(FL*2)/(rho*A*(V^2));
+disp("Coefficient Of Lift ="+string(Cl)+" No Units");
+disp("Coefficient Of Drag ="+string(Cd)+" No Units");
diff --git a/2021/CH16/EX16.5/EX16_5.pdf b/2021/CH16/EX16.5/EX16_5.pdf
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diff --git a/2021/CH16/EX16.5/EX16_5.sce b/2021/CH16/EX16.5/EX16_5.sce
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+//Finding of Weight
+//Given
+D=0.05;
+v=1.5*10^-4;
+V=10;
+rho=1.25;
+Cd=0.5;
+//TO Find
+A=(%pi/4)*D^2;
+Fd=Cd*rho*A*((V^2)/2);
+disp("Weight of the ball ="+string(Fd)+" Newtons");
diff --git a/2021/CH16/EX16.6/EX16_6.pdf b/2021/CH16/EX16.6/EX16_6.pdf
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diff --git a/2021/CH16/EX16.6/EX16_6.sce b/2021/CH16/EX16.6/EX16_6.sce
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+//Finding of Circulation,Theoretical Drag,Actual Drag,Lift,Resultant,Direction
+//Given
+V=20;
+D=2;
+A=2*10;
+R=D/2;
+N=300;
+L=10;
+Cd=0.65;
+Cl=3.4;
+rho=1000;
+//To find
+Vp=(%pi*D*N)/60;
+//case 1
+C=2*(%pi)*R*Vp;
+disp("Circulation ="+string(C)+" m^2/sce");
+//case 2
+Fl=rho*V*L*C;
+disp("Theoretical Lift ="+string(Fl)+" Newtons");
+//case 3
+si=C/(4*(%pi)*V*R);
+theta1=(180+si);
+theta2=(360-si);
+disp("theta ="+string(theta1)+" Degrees");
+disp("theta ="+string(theta2)+" Degrees");
+//case 3
+FL=0.5*rho*A*V^2*Cl;
+disp("Lift Force ="+string(FL)+" Newtons");
+//case 4
+FD=0.5*rho*A*(V^2)*Cd;
+disp("Drag Force ="+string(FD)+" Newtons");
+//case 5
+F=sqrt((FL^2)+(FD^2));
+disp("Resultant Force ="+string(F)+" Newtons");
+//case 6
+theta=1/tan(FL/FD);
+disp("Direction ="+string(theta)+" Degrees");
+//case 7
+C1=4*(%pi)*V*R;
+Vp=C1/(2*(%pi)*R);
+N=(Vp*60)/(2*(%pi));
+disp("Speed ="+string(N)+" rpm");