So for Module 7 this is the data that I ran. I need a little
guidance on this second part. Here is my Matlab code below for the
first module:
%define load
P=[0:1:600];% p=0,1,2,3...600 lb p will take these values
%define other dimensions
c=0.4; G=4000;L=6.32;b=1.8;
%computing displacement using u=Pc/(GLb) inches
u=(P*c)./(G*L*b);
%plotting displacement (u) vs load(P)
figure(1)
plot(u,P,'r--');
%computing shear stress tau=P/Lb
tau=P./(L*b);
%plotting shear stress (tau) vs Load (P)
figure (2)
plot(tau,P,'g--');
%computing shear strain shear=u/c
shear_strain=u./c;
%plotting shear strain vs displacement (u)
figure (3)
plot(shear_strain,u,'m--');
Now I need to find the following: (Should be several test
runs)
Continuing from Module 7 discussion; now adjust your model by
using “W” direction properties and these adjusted dimensions:
thickness 0.40 inch (narrow thickness) and 1.2 inch (wide
thickness), width 1.80 inches and length 6.32 inches. Note the
modified SolidWorks image below; the scalloped section seen on the
right of the honeycomb sample is 0.3-inch diameter and this area
should be removed from both ends of the sample.
The below plot was generated from an actual C273 test (ASTMCompass/ERAU). e of a compression specimen fabricated with the above dimensions. Load versus Extension 560 480 400 [296] Test Run 2 Test Run 3 Test Run 4 Test Run 5 Test Run 6 Test Run 7 Test Run 8 Test Run 9 Test Run 10 Test Run 11 320 Load (lb) 240 160 80 0 80 -0.07 -0.03 0.01 0.05 0.13 0.17 0.21 0.25 0.09 Extension (in) You are to complete the following: 1. Model, analyze, and plot (1st plot) your work from module 7 with the new specimen dimensions and properties. 2. Adjust (transform) your model to accommodate for a test misalignment error noted in the fixture of 3 degrees (eccentric loading state) and correct (2nd plot) your 1st. 3. State, with supporting equation, at what stress will an individual honeycomb cell deform and buckle? 4. Reflect and Think: why do additional test runs of the same specimen produce the observed results as seen in the above plot of
The below plot was generated from an actual C273 test (ASTMCompass/ERAU). e of a compression specimen fabricated with the above dimensions. Load versus Extension 560 480 400 [296] Test Run 2 Test Run 3 Test Run 4 Test Run 5 Test Run 6 Test Run 7 Test Run 8 Test Run 9 Test Run 10 Test Run 11 320 Load (lb) 240 160 80 0 80 -0.07 -0.03 0.01 0.05 0.13 0.17 0.21 0.25 0.09 Extension (in) You are to complete the following: 1. Model, analyze, and plot (1st plot) your work from module 7 with the new specimen dimensions and properties. 2. Adjust (transform) your model to accommodate for a test misalignment error noted in the fixture of 3 degrees (eccentric loading state) and correct (2nd plot) your 1st. 3. State, with supporting equation, at what stress will an individual honeycomb cell deform and buckle? 4. Reflect and Think: why do additional test runs of the same specimen produce the observed results as seen in the above plot of
So for Module 7 this is the data that I ran. I need a little guidance on this second part. Here is my Matlab code below
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answerhappygod
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So for Module 7 this is the data that I ran. I need a little guidance on this second part. Here is my Matlab code below
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