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authorprashantsinalkar2017-10-10 12:27:19 +0530
committerprashantsinalkar2017-10-10 12:27:19 +0530
commit7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch)
treedbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /1586/CH14
parentb1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff)
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+clc;funcprot(0);//EXAMPLE 14.1
+// Initialisation of Variables
+d1=0.5;..........//Diameter of a steel Cable in in.
+rhoy=70000;........//Yield Strength of Steel Cable in psi
+rhoa1=36000;........//Yield Strength of Aluminum in psi
+rhos=0.284;..........//Density of Steel in lb/in^3
+rhoa2=0.097;.........//Density of Aluminum in lb/in^3
+//CALCULATIONS
+F=rhoy*((%pi/4)*(d1^2));........//Load applied on Aluminum in lb
+d2=sqrt((F/rhoa1)*(4/(%pi)));.......//Diameter of Aluminum in in.
+Ws=(%pi/4)*(d1^2)*12*rhos;..........//Weight of Steel in lb/ft
+Wa=(%pi/4)*(d2^2)*12*rhoa2;..........//Weight of Aluminum in lb/ft
+disp(F,"a. Load applied on Aluminum in lb:")
+disp(d2,"b. Diameter of Aluminum in in.: ")
+disp(Ws,"c. Weight of Steel in lb/ft:")
+disp(Wa,"Weight of Aluminum in lb/ft:")
diff --git a/1586/CH14/EX14.4/EXP14_4.jpg b/1586/CH14/EX14.4/EXP14_4.jpg
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+clc;funcprot(0);//EXAMPLE 14.4
+// Initialisation of Variables
+K=567.53*10^6;..........//Slope of the Equationof Mg- alloy in Pa-nu/m^2
+d=10;...........//Grain size in nu-m
+Y=52.54*10^6;...........//Intercept of Mg- alloy in Pa
+//CALCULATIONS
+Yp=Y+(K*d^(-1/2));.......//Predicted yield strength of an Mg- alloy in MPa
+disp(Yp,"Predicted yield strength of an Mg- alloy in MPa:")
diff --git a/1586/CH14/EX14.6/EXP14_6.jpg b/1586/CH14/EX14.6/EXP14_6.jpg
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+clc;funcprot(0);//EXAMPLE 14.6
+// Initialisation of Variables
+%A=10;.......//Percentage of Alloy in Cu-Al alloy
+%M=9.4;.......//Percentage of Martensite present in Cu-Al alloy
+%Fe=15.6;......//Percentage of Ferrite present in Cu-Al alloy
+//CALCULATIONS
+%a=((%A-%M)/(%Fe-%M))*100;....//Percentage of Austenite forms at 400 degree celsius in Cu-Al alloy
+disp(%a,"Percentage of Austenite forms at 400 degree celsius in Cu-Al alloy")
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+clc;funcprot(0);//EXAMPLE 14.8
+// Initialisation of Variables
+Ktc=60;.........//The plane-strain Fracture toughness in MPa-m^-1/2
+Ktc2=80;......//The fracture toughness of L sample in MPa-m^-1/2
+f=1.12;........//A geometry factor for the specimen and flaw
+sigma=200;......//A titanium-alloy 6246 plate is exposed to a tensile stress
+a=((Ktc/(f*sigma))^2)/%pi;......//The critical flaw length of Crank in cm
+a2=((Ktc2/(f*sigma))^2)/%pi;......//The critical flaw length of Crank of L sample in cm
+disp(a*10^2," The critical flaw length of Crank in cm: ")
+disp(a2*10^2,"The critical flaw length of Crank of L sample in cm:")