![]() |
||||||||||||||||||||||||||||||
Beam Deflections Analysis |
||||||||||||||||||||||||||||||
|
|
||||||||||||||||||||||||||||||
|
|
Serviceability of a structure is determined by its deflection, cracking, extend of corrosion, and surface deterioration. Excessive deflection of a beam or slab can damage a partition below, and excessive deflection of a lintel beam above a window opening can crack the glass panes. The program computes the maximum deflection of a simply
supported double-reinforced concrete rectangular or T beam under the action
of service loads, taking into account the immediate and the long-term
effects, according to ACI design criteria. In addition, continuous beams
or one-way slabs may also be modeled by entering the corresponding end
moments. |
|||||||||||||||||||||||||||||
|
ASDIP Programs:
Base Plates
Beam Deflections Cantilever Footings Composite Beams Corbels / Beam Ledges Deep Beams Circular Columns Rectangular Columns Any-shaped Shear Walls Lateral Load Distribution Masonry Walls Web Openings Pile Foundations Retaining Walls Spread Footings Steel Beams Steel Columns Floor Vibrations Concrete Beams Seismic Shear Walls |
ExampleFind the maximum deflection of a uniformly loaded continuous beam with
four spans of 36 ft., a width of 14 in. and a total depth of 21-in. supporting
a 4" slab. The steel area is 4.00 in2 at a depth of 18.25 in. The
beam is subjected to a service dead load of 700 plf including its self-weight
and a live load of 1200 plf. Use f'c = 4 ksi and fy = 60 ksi. Assume that
50% of the live load is continuously applied. |
|||||||||||||||||||||||||||||
Input DataThe required input data consists of the materials' properties and beam dimensions. In addition, the service dead and live loads (a distributed load and two end moments) are required, as shown schematically in the figure below. |
||||||||||||||||||||||||||||||
![]() |
||||||||||||||||||||||||||||||
![]() |
||||||||||||||||||||||||||||||
ProcedureThe program computes the section's properties in the pre-cracking and post-cracking stages and calculates the effective moment of inertia based on the Branson approach. The maximum deflection is computed as the sum of the instantaneous deflection and the long-term deflection in accordance with the ACI procedure. It is then compared with maximum values allowed, depending on the type of structure. ASDIP generates the bending moment diagram of the designed beam for the specified service loads, as shown below. |
||||||||||||||||||||||||||||||
OutputFigure below shows the template related to this module with the example problem's data. In this example, the code deflection criterion is met by conditions A and B only. Therefore, the continuous beam is limited to floors or roofs not supporting or attached to nonstructural elements such as partitions. |
||||||||||||||||||||||||||||||
![]() |
||||||||||||||||||||||||||||||
![]() |
||||||||||||||||||||||||||||||
|
|
||||||||||||||||||||||||||||||
|
||||||||||||||||||||||||||||||
Copyright © 2008 by ASDIP Structural Software - ALL RIGHTS RESERVED P.O. Box 608723 Orlando, FL 32860 Phone 407-284-9202 E-mail: support@asdipsoft.com |
||||||||||||||||||||||||||||||