# Matplotlib compatibility patch for Pyodide
import matplotlib
if not hasattr(matplotlib.RcParams, "_get"):
matplotlib.RcParams._get = dict.get
Exam Monday April 14th#
Today you’ll make the third exam assignment covering Statically indeterminate structures including its prerequisites and/or the third exam assignment covering Continuum mechanics including its prerequisites and/or the second exam assignment covering Buckling including its prerequisites. For more information about the exam see the assessment information in course information
Exam assignment 3 Statically indeterminate structures#
Your own submission and its grading can be found here: exam assignment Statically indeterminate structures 3. The exam assignment was provided as follows:
Given is the structure as shown in the figure below.
Calculate the normal force- and bending moment distribution using a force-, displacement- or hybrid- (‘hoekveranderingsvergelijkingen’ with moveable nodes) method.
Solution
Convert the structure into a statically determinate structure with a displacement or force condition.
For example when using the force method:
Using forget-me-nots, the displacement in A can be described as:
\(w_\text{A} = \cfrac{36}{25} - {24}{625} A_v \)
\(u_\text{A} = 15 - \cfrac{3}{10} A_h\)
With the requirements of no displacement, this results in:
\(A_v = -37.5 \text{ kN}\)
\(A_h = -50 \text{ kN}\)
This gives the normal force and bending moment distribution:
Exam assignment 3 Continuum mechanics#
Your own submission and its grading will be available on exam assignment Continuum mechanics 3 after the exam.
Given is the following structure:
Find the stresses alongside all edges of the stress shown element from the point E in the cross-section just to the left of D in element CD.
Evaluate whether the stress element fails according to Von Mises’ failure criterium.
Solution
In the cross-section, the bending moment is \(0\). The normal force is \(54 \text{ kN}\) and the shear force \(72 \text{ kN}\)
Relevant cross-sectional properties are:
\(A = 10800 \text{ mm}^2\)
From top fibre downwards, the normal force centre is at \(200 \text{ mm}\)
\(I_{zz} = 108043200 \text{ mm}^4\)
This gives in E:
\(\sigma = 5 \text{ MPa}\)
\(\tau \approx 10 \text{ MPa}\)
The stresses on the stress element can be calculated using the transformation formulas or using Mohr
This leads to:
\(\sigma_1 = 12.8 \text{ MPa}\)
\(\sigma_2 = -7.80 \text{ MPa}\)
and the following stresses on the stress-element:
The required yield stress results according to Von Mises is: \(\sqrt{\cfrac{1}{2}\left( \left(12.8+7.8 \right)^2 + 12.8^2 + \left(-7.8\right)^2 \right) } = 12.7 \text{ MPa}\), so the point does not fail.
Exam assignment 2 Buckling#
The exam assignment was provided as shown here
Solution
The solution is shown here