Continuous and Single Beam Analysis Spreadsheet

 

Structural analysis of a single-span or continuous-span beam requires determination of the internal loading distribution based on external loads and beam supports. This workbook provides the calculations necessary for determination of the internal loading distribution (shear and moment distribution) along with the slope and deflection distribution. The Workbook by Mr. Tomanovich is mainly for steel structures in the Civil Engineering world.  I am in Aerospace and deal in inches and millimeters rather than feet. Therfore, I have tried to make the calculations unit free.

Program Description:
This Workbook provides  for the analysis of either single-span or two (2) to five (5) continuous-spans analysis a beam with loadings including point loads, point moments, constant distributed and linearly variable loadings.  Four (4) end constaint cases for the single-span beam, and fixed or simple support at ends of the two (2) through (5) span, continuous-span beam, are considered.  Specifically, beam end reactions as well as the maximum moments and deflections are calculated.  Plots of both the shear and moment diagrams are produced, as well as a tabulation of the shear, moment, slope, and deflection for the beam or each individual span.

This Excel Workbook consists of four (4) Worksheets, described as follows:
Doc – This documentation sheet
Single-Span Beam – Single-span beam analysis for simple, propped, fixed, & cantilever beams
Continuous-Span Beam – Continuous-span beam analysis for 2 through 5 span beams
Reference – Formulas and Methods used in the calculations

Program Assumptions and Limitations:

1.   The following reference was used in the development of this program (see below):
“Modern Formulas for Statics and Dynamics, A Stress-and-Strain Approach” by Walter D. Pilkey and Pin Yu Chang, McGraw-Hill Book Company (1978), pages 11 to 21.
2.   This Workbook uses the three (3) following assumptions as a basis for analysis:
a.  Beams must be of constant cross section (E and I are constant for entire span length).
b.  Deflections must not significantly alter the geometry of the problem.
c.  Stress must remain within the “elastic” region.
3.   On the beam or each individual span, this Workbook will handle a full length uniform load and up to eight (8) partial uniform, triangular, or trapezoidal loads, up to fifteen (15) point loads, and up to four (4) applied moments.
4.   For single-span beams, this Workbook always only allows a particular orientation for two (2) of the the four (4)
different types.  Specifically, the fixed end of either a “propped” or “cantilever” beam is always assumed to be on
the right end of the beam.
5.   This Workbook will calculate the beam end vertical reactions and moment reactions (if applicable), the maximum positive moment and negative moment (if applicable), and the maximum negative deflection and positive deflection (if applicable).  The calculated values for the end reactions and maximum moments and deflections are determined from dividing the beam into fifty (50) equal segments with fifty-one (51) points, and including all of the point load and applied moment locations as well.  (Note: the actual point of maximum moment occurs where the shear = 0, or passes through zero, while the actual point of maximum deflection is where the slope = 0.)
6.   Calculations for two (2) specific locations from the left end of the beam for the shear, moment, slope, and deflection is available.
7.   The plots of the shear and moment diagrams as well as the displayed tabulation of shear, moment, slope, and deflection are based on the beam (or each individual span) being divided up into fifty (50) equal segments with fifty-one (51) points.
8.   For continuous-span beam of from two (2) through five (5) spans, this program utilizes the “Three-Moment Equation Theory” and solves a system simultaneous equations to determine the support moments.
9.  This Workbook contains numerous “comment boxes” which contain a wide variety of information including explanations of input or output items, equations used, data tables, etc.  (Note:  presence of a “comment box” is denoted by a “red triangle” in the upper right-hand corner of a cell.  Merely move the mouse pointer to the desired cell to view the contents of that particular “comment box”.)

 

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Beam Analysis with FEM Excel Sheet

 

 

Beam Analysis with FEM Excel Sheet is an application of MS-Excel “Solver” to Non-linear Beam Analysis written by Toshimi Taki Prepared on March 4, 2007

There are some types of beam structures as shown in figure 1.

Figure 1 : Types of Beam Structures

If beam elements of “simple beam” structures are subject to lateral load only, this type of beam structure shows linear behaviour. “Simple beam” structures can be analysed easily. When beam elements in a beam structure are subject to lateral load and axial load, the structure shows non-linear behaviour.

The examples of the non-linear beam problems are beam columns, Elastica and arch structures. Analytical method is applicable only to idealized structures such as uniform cross section beam column.

You need to use non-linear finite element analysis to solve non-linear beam structures in real world. I have developed a new method to solve non-linear beam structures.

This is a direct application of energy principle using MS-Excel “Solver”. Application of MS-Excel “Solver” to Non-linear Beam Analysis “Elastica” is used as an example to show the method. Following figures show the results.

Figure 2 :  Model for Elastica

 

Figure 3 :  Result — Deflection

 

Figure 4 : Result — Load-Deflection Curve

 

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Base Isolated Building Design Excel Sheet

 

DESIGN CRITERIA

1. Base isolator system can reduce seismic loads by increasing the period/reducing the stiffness of structure. But the building wind loads are the same without change. So not all structures are adequate for base isolator system, with both seismic and wind limits.

2. The period of fixed-base structure and building wind load can be calculated by 3D finite element method (FEM) and spreadsheets.

But it is very difficult to use finite elements modeling isolators, since damping and isolator stiffness matrix. This design method, using building effective stiffness concept for entire structure and isolated system, to check if the structure is adequate for base isolator system. If adequate, users can select and test isolated system by wind loads to drift limits (ASCE 7-16/10 17.2.4.2 & 17.5.6).

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