Brief data for post 3 -steel beam

3- An Easy Introduction to Plastic Theory for Beams.

What is Plastic Theory? Video.

The video discusses the Plastic Theory, in which the idea of an idealized Stress-strain curve is introduced. what is the relation between stress and stress and how we can get the plastic hinge? The video has a closed caption and subtitles in English.

The topics included in our discussion are shown in the next slide. The various regions are shown the relation between stress and strain for mild steel under tension.
The elastic design utilizes the linear portion of the graph, the upper and lower fibers of the section will have f=Fy.

Notice: I have added extra data in the post more than in the video.

Allowable working stress design method AWSD, quick revision.

We will start to review the allowable working stress design method in which the compression force acts at a distance of (1/3)*d/2=d/6 from the upper fiber of the section, while the Tension force acts at a distance of d/6 from the lower fiber.

The lever arm of C or T =((d-2*(1/6))=2/3d, which is the distance between the points of application between the compressive force C and the tensile force T and sometimes called Yct is the compression and tension, Yct =2/3d.

The Moment value =f(*b*d^2/6), the value of (b*d^2/6) is called elastic section modulus and denoted by the symbol S. So the moment can be expressed as the product of f*S.

The relation between stress and strain.

The stress distribution diagram for a section is shown when the design is based on the working stress with a maximum value at the extreme upper fibre=fb. the distribution as shown is linear and the stress value is zero at the neutral axis.

Stress-moment relationship and forces.

The moment of resistance of the section can be estimated from the value of Fb and the section modulus S which is the inertia/(h/2) for a rectangular section where h is the overall height of the section.
Again the moment is  MR= Fb*S. the maximum stress value for the compact section was considered as =0.66Fy.

The relation between elastic section and Working moment for compact and non-compact sections

Allowable stress relation with the moment

This is more detail regarding the relationship between Moment and working stress and how to derive the expression.

The triangular stress was converted into two equal forces acting at (2/3 )of (d/2) from the neutral axis, creating a moment equal to the product of T*Yct or c*yct, where yct is the distance between the point of applications of C&T forces.

Considering the elastic section modulus x as the value of (I/y), we can derive the final expression.

The moment value acting on the section in terms of the stress .

The Moment stress relationship in case of compact or non compact section.

to the Plastic Theory.

The plastic theory has considered that at the places of maximum moments, the section can be regarded as carrying stresses equal to yield stress, which will lead to a formation of plastic hinges; at these plastic hinges, there will be no ability to take further load and collapse will develop.

The following assumptions are made per the next plastic theory slide.
1-the stress-strain relationship is idealized into two straight lines,s as shown in the figure.
2- The plane section before bending remains the plane even after bending.

The assumptions of the plastic theory

3-The relationship between compressive stress and compressive strain is the same as between tensile stress and tensile strain.
4-Whenever a plastic moment is attained -at any cross section-a plastic hinge forms which can undergo rotation of any magnitude, but the bending moment remains constant at the fully plastic value.

5-Effect of axial load and shear on the fully plastic moment capacity of the section are neglected.
6-The deflections in structures are small enough for the equations of statical equilibrium to be the same as those for the undeformed structures.

The stain value at the plastic stage/strain at the yield stage is approximately 10. the strain at the plastic stage can be set to 1.50*1/100 as shown in the next picture.

The idealized stress-strain graph.

The next slide shows the stages for a rectangular section under applied loads, at the elastic stage where the extreme upper and lower fibers have reached Fy, this is called the elastic stage.

Next, under increasing loads, the stresses at the extreme fibers cannot exceed Fy, then the lower fibers will develop stress equal to Fy, but some fibers have not reached Fy, this stage is called elastic-plastic.

At the plastic stage, after a further increase in loads, all the rectangular section fibers have been stressed to Fy and the moment that the section can carry the plastic moment, please refer to the next picture.

The formula used to get the value of the plastic section modulus Zx.

This is the pdf file used for the illustration of this post.

This is a link to a good source for steel beams.

This is the link to the
next post, what are Elastic and plastic section moduli?

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