summaryrefslogtreecommitdiff
path: root/3776/CH11/EX11.11
diff options
context:
space:
mode:
Diffstat (limited to '3776/CH11/EX11.11')
-rw-r--r--3776/CH11/EX11.11/Ex11_11.sce59
1 files changed, 59 insertions, 0 deletions
diff --git a/3776/CH11/EX11.11/Ex11_11.sce b/3776/CH11/EX11.11/Ex11_11.sce
new file mode 100644
index 000000000..510361b42
--- /dev/null
+++ b/3776/CH11/EX11.11/Ex11_11.sce
@@ -0,0 +1,59 @@
+clear
+//
+P = 200.0 //K The force on the beam
+L = 15 //ft - The length of the rod
+F_y = 50.0 //ksi
+F_a = F_y/(5.0/3) //ksi -AISC MANUAL ,allowable axial stress if axial force is alone
+F_b = F_a //Allowable compressive bending stress
+M_1 = 600.0 //k-in - The moment acting on the ends of the rod
+M_2 = 800.0 //k-in - the moment acting on the other end of teh rod
+B_x = 0.264 //in - Extracted from AISC manual
+E = 29*(10**3)
+A = P/F_a + M_2*B_x/F_b //in2- The minimum area
+printf("\n \n The minimum area is %0.2f in^2",A)
+//we will select W10x49 section
+A_s = 14.4 //in2 - The area of the section
+r_min = 2.54 //in The minimum radius
+r_x = 4.35 //in
+f_a = P/A_s //Ksi- The computed axial stress
+f_b = M_2*B_x/A_s //Computed bending stess
+C_c = ((2*(%pi**2)*E/F_y)**0.5) //Slenderness ratio L/R
+C_s = L*12/r_min // Slenderness ratio L/R of the present situation
+if C_s <C_c then
+ printf("\n The following approch is solvable")
+else
+ printf("\n The caliculation is not possible")
+ end
+F_a_1 = 19.3 //Ksi - AISC lets try this
+c_m = 0.6 - 0.4*(-M_1/M_2)
+F_e = (12*(%pi**2)*E)/(23*(L*12/r_x)**2)
+k = f_a/F_a_1 + c_m*f_b*(1-(f_a/F_e))/F_b //Condition mentioned in AISC
+if k>1 then
+ printf("\n The following W10x49 section is not satisfying our constraints since f_a/F_a_1 + c_m*f_b*(1-(f_a/F_e))/F_b %0.3f >1",k)
+else
+ printf("\n The following W10x49 section is satisfying our constraints since f_a/F_a_1 + c_m*f_b*(1-(f_a/F_e))/F_b %0.3f <1",k)
+ end
+//trail - 2
+//Lets take W10 x 60
+A_s = 17.6 //in2 - The area of the section
+r_min = 2.57 //in The minimum radius
+r_x = 4.39 //in
+f_a = P/A_s //Ksi- The computed axial stress
+f_b = M_2*B_x/A_s //Computed bending stess
+C_c = ((2*(%pi**2)*E/F_y)**0.5) //Slenderness ratio L/R
+C_s = L*12/r_min // Slenderness ratio L/R of the present situation
+if C_s <C_c then
+ printf("\n The following approch is solvable")
+else
+ printf("\n The caliculation is not possible")
+ end
+F_a_1 = 19.3 //Ksi - AISC lets try this
+c_m = 0.6 - 0.4*(-M_1/M_2)
+F_e = (12*(%pi**2)*E)/(23*(L*12/r_x)**2)
+k = f_a/F_a_1 + c_m*f_b*(1-(f_a/F_e))/F_b //Condition mentioned in AISC
+if k>1 then
+ printf("\n The following W10x49 section is not satisfying our constraints since f_a/F_a_1 + c_m*f_b*(1-(f_a/F_e))/F_b %0.3f >1",k)
+else
+ printf("\n The following W10x49 section is satisfying our constraints since f_a/F_a_1 + c_m*f_b*(1-(f_a/F_e))/F_b %0.3f <1",k)
+ end
+printf("\n small variation due to rounding off errors") \ No newline at end of file