From 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 Mon Sep 17 00:00:00 2001
From: prashantsinalkar
Date: Tue, 10 Oct 2017 12:27:19 +0530
Subject: initial commit / add all books

---
 3705/CH11/EX11.2/Ex11_2.sce | 26 ++++++++++++++++++++++++++
 1 file changed, 26 insertions(+)
 create mode 100644 3705/CH11/EX11.2/Ex11_2.sce

(limited to '3705/CH11/EX11.2/Ex11_2.sce')

diff --git a/3705/CH11/EX11.2/Ex11_2.sce b/3705/CH11/EX11.2/Ex11_2.sce
new file mode 100644
index 000000000..dccd269c2
--- /dev/null
+++ b/3705/CH11/EX11.2/Ex11_2.sce
@@ -0,0 +1,26 @@
+
+clear//
+
+//Variable Declaration
+V=1000 //Shear Force in lb
+t=0.5 //Thickness in inches
+wf=12 //Width of the flange in inches
+d=8 //Depth of the section in inches
+//Rest ALL DATA is similar to previous problem
+
+//Calcualtions
+I=t*wf**3*12**-1+t*d**3*12**-1 //Moment of Inertia
+
+//Part 1
+q1=V*t*t*wf*3*I**-1 //Shear Flow in lb/in
+q2=V*t*t*d*2*I**-1 //Shear FLow in lb/in
+V1=2*3**-1*q1*wf //Shear force carried in lb
+V2=2*3**-1*q2*d //Shear force carried in lb
+
+//Part 2
+e=8*V2*V**-1 //Eccentricity in inches
+
+//Result
+printf("\n The Shear Force carried by Flanges is")
+printf("\n Top Flange= %0.1f lb Bottom Flange= %0.1f lb",V1,V2)
+printf("\n The eccentricity is %0.3f in",e)
-- 
cgit