Staircases provide simple solutions for vertical circulation in a building. In this post, we are going to model a simple staircase using finite element plates, and compare the answer with manual calculations in which we assume the staircase to be a simply supported beam. The aim of this post is to verify the results obtained from the different procedures, and give reinforced concrete designers a little idea about the results to expect from their assumptions.
Let us consider a section of a staircase with dimensions as shown below;
|Fig 2: Section of Staircase|
The loading on the staircase is as follows;
Ultimate load on the flight = 15.719 kN/m2
Ultimate load on the landing = 14.370 kN/m2
Width of staircase = 1000 mm
Analysis Using Staad Pro (3D Finite Element Plate Model)
The 3D Model of the staircase is as given below;
|Fig 3: Rendered 3D Model of the Staircase|
(1) Modelling the staircase as 3D Plate with pinned-pinned supports
|Fig 4: Model of the staircase with pinned-pinned support|
The static analysis of the structure gave the result below;
|Fig 5: Transverse Bending Moment on the Staircase (Mx)|
|Fig 6: Longitudinal Bending Moment (My) on the Staircase|
(2) Modelling the Staircase as 3D plate with pinned-roller support;
|Fig 7: Modelling the Staircase with Pinned-Roller Support|
The analysis result gave the following;
|Fig 8: Transverse Bending Moment (Mx)|
|Fig 9: Longitudinal Bending Moment (My)|
(3) Modelling the staircase as a static 2D frame with pinned-pinned support;
|Fig 10: Bending moment on the Staircase (Frame Model; pinned-pinned support)|
(4) Modelling the staircase as a 2D frame with pinned-roller support
|Fig 11: Bending Moment on the staircase (pinned-roller model)|
(5) Modelling the staircase as a simply supported beam
|Figure 12: Bending Moment on the stair (simply supported beam model – horizontal length)|
Discussion of Results
(1) The analysis results using the above named methods gave all the bending moments in the staircase to be sagging.
(2) Finite element plate model gave the maximum sagging at the flight to be 41.1 kNm (see Fig 5), while the maximum sagging moment on the landing was found to be 32.6 kNm (see Fig 6). This result was found in both pinned-pinned model and pinned-roller model, therefore, there is no difference in using any of the support conditions in Staad Pro.
(3) Static 2D frame model of the staircase gave the maximum sagging moment on the flight to be 41.1 kNm, while the maximum sagging moment on the flight was 33.82 kNm (see Fig 10 and 11). In principle, it can be said there is no difference in modelling the staircase as a simple 2D frame or as a 3D plate model. The former is more economical time wise.
(4) The model of span dimension adopted for the manual equivalent beam calculation was picked from SCALE software, and the maximum moment on the flight was found to be 36.04 kNm (see Fig 12). This is about 12.3% less than other models. A little consideration will show that this effect stems from the span dimensions.
To take care of this, let us modify the flight dimensions as follows;
Lf,m = Lf/cos ϕ
Where Lf is the horizontal span of flight, Lf,m is the actual length of the flight, and ϕ is the angle of inclination of the flight.
Thus; Lf,m = 1.75m/cos 34.4 = 2.12m
This gave the result below;
|Fig 13: Bending moment on the stair (simply supported beam model, developed length)|
We can see that is more comparable and conservative when compared with results from computer models. Therefore, for all simple staircases, we can use the developed length of the flight instead of the horizontal length to analyse the staircase as a simply supported beam. However when checking for deflection, we should use the horizontal length.
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