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+clc
+//
+//
+
+//Variable declaration
+Sy=36 // Stress(ksi)
+E=(29*((10**6))) // Modulus of elasticity(psi)
+A=11.5 // Area(in**2)
+FS=2 // Factor of safety
+
+
+//Calculation
+ratio=(4.71)*(E/(36*((10**3)))) // Value of the slenderness ratio
+
+//Case(a) Effective Length
+Sr=(24*12)/(1.98) // Value of the slenderness ratio
+Scr=((0.877)*((%pi)**2)*(29*((10**3))))/(145.5)**2 // Value of the slenderness ratio
+Sall=(Scr/1.67) // Allowable stress(ksi)
+Pall1=Sall*A // Pressure(kips)
+//Case(b) Bracing at Midpoint C
+//xz Plane
+Elxz=(144)/(1.98) // Slenderness ratio
+//yz Plane
+Elyz=(288)/(4.27) // Slenderness ratio
+
+Se=(((%pi)**2)*(E))/(72.7)**2 // Stress(ksi)
+Scr=(0.658)**(36/54.1)*(36) // Stress(ksi)
+
+Sall=(Scr)/(1.67) // Allowable load(ksi)
+Pall2=Sall*A // Force(ksi)
+
+//Result
+printf("\n Effective centric load P if the effective length of the column is 24 = %0.3f kips",Pall1)
+printf("\n Effective centric load P if bracing is provided to prevent the movement of the midpoint C in the xz plane = %0.3f ksi",Pall2)