/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 12 A wood beam \(A B C\) with simpl... [FREE SOLUTION] | 91Ó°ÊÓ

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A wood beam \(A B C\) with simple supports at \(A\) and \(B\) and an overhang \(B C\) has height \(h=300 \mathrm{mm}\) (see figure). The length of the main span of the beam is \(L=3.6 \mathrm{m}\) and the length of the overhang is \(L / 3=1.2 \mathrm{m}\). The beam supports a concentrated load \(3 P=18 \mathrm{kN}\) at the midpoint of the main span and a moment \(P L / 2=10.8 \mathrm{kN} \cdot \mathrm{m}\) at the free end of the overhang. The wood has weight density \(\gamma=5.5 \mathrm{kN} / \mathrm{m}^{3}\) (a) Determine the required width \(b\) of the beam based upon an allowable bending stress of \(8.2 \mathrm{MPa}\) (b) Determine the required width based upon an allowable shear stress of \(0.7 \mathrm{MPa}\)

Short Answer

Expert verified
Calculate beam width for bending as \( b = 1.39 \text{ m} \). Shear width \( b = 0.285 \text{ m} \). Use the larger width, \( b = 1.39 \text{ m} \).

Step by step solution

01

Understand the Problem

We are tasked to find the width \(b\) of a beam given specific constraints on allowable bending and shear stresses in a system with a wood beam \(A B C\), with certain loads applied. The key elements include the beam heights, the main span length, overhang length, load and moment, and given mechanical properties such as stresses and density.
02

Calculate the Design Bending Stress

The bending stress \(\sigma\) is given by the formula \(\sigma = \frac{M}{Z}\), where \(M\) is the bending moment and \(Z\) is the section modulus. The maximum moment occurs at the midpoint of the main span due to the load, calculated as \(M = \frac{3P \cdot L}{4} = 16.2 \text{ kN} \cdot \text{m} = 16200 \text{ Nm}\). The section modulus is \(Z = \frac{1}{6} bh^2\). Solving for \(b\), with \(\sigma = 8.2 \text{ MPa}\), gives \(b = \frac{6M}{\sigma h^2}\). Substitute the values to find \(b\).
03

Calculate the Design Shear Stress

The maximum shear force occurs at the supports due to the applied load. Shear stress \(\tau\) is calculated as \(\tau = \frac{V}{Q}\), where \(V\) is the shear force and \(Q\) is the first moment of area. The formula for \(Q\) for a rectangular beam is \(\frac{1}{2}bh\cdot\frac{h}{2}\). The shear force \(V\) can be found from equilibrium considerations. Solving for \(b\), with \(\tau = 0.7 \text{ MPa}\), gives \(b = \frac{3V}{\tau h}\). Calculate \(b\) using the provided values.
04

Compare the Results to Ensure Safety

Compute the required widths \(b\) for both bending and shear conditions. The greater of these widths will ensure that the beam is safe against both bending and shear failure. Verify your calculations to ensure they meet the conditions given in the problem.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Bending Stress in Beam Design
When designing beams, bending stress is a crucial factor that must be considered to ensure structural integrity. Bending stress occurs when an external load is applied to a beam, causing it to bend. The stress increases with the magnitude of the load and can lead to failure if not properly managed.
This stress, denoted as \( \sigma \), is calculated using the formula \( \sigma = \frac{M}{Z} \), where \( M \) is the bending moment and \( Z \) is the section modulus. In this exercise, the maximum moment \( M \) is determined based on the load distribution along the beam, specifically at the midpoint of the main span.
  • Maximize section modulus \( Z \) by adequately designing the beam's cross-section.
  • Bending stress should never exceed material's allowable limit, \( 8.2 \text{ MPa} \) in this case.
Calculating the proper width \( b \) ensures the beam can withstand the bending stress without failure. It’s computed as \( b = \frac{6M}{\sigma h^2} \), ensuring that the design constraints are met.
Understanding Shear Stress
Shear stress is another critical aspect of beam design, referring to the internal forces that parallel the cross-sectional area. It occurs when parts of the beam slide past each other due to the applied loads.
In engineering, shear stress, \( \tau \), is found using \( \tau = \frac{V}{Q} \), where \( V \) is the shear force reaching maximum at the supports, and \( Q \) is the first moment of the area.
  • To prevent shear failure, the beam's width \( b \) should be calculated to keep shear stress below the allowed \( 0.7 \text{ MPa} \).
  • Use \( b = \frac{3V}{\tau h} \) to determine this width, ensuring the beam's capacity for shear force is not exceeded.
Understanding these calculations will help ensure that the beam sustains its structural function safely.
Design of Wood Beams
Wood beams are utilized extensively in construction due to their strength and aesthetics. However, they must be precisely designed to withstand stresses from loads and moments.
To achieve a safe design, various factors must be considered:
  • The height \( h \) and width \( b \) of the beam impact its structural capacity.
  • Wood's density, given as \( \gamma = 5.5 \text{ kN/m}^3 \), plays a role in calculating self-weight and load impacts.
The primary goal is to ensure that the wood beam manages bending and shear stresses effectively without compromising safety. This involves not only looking at the maximum stress the material can withstand but also understanding how the beam will behave under different loading conditions.
Overview of Structural Analysis
Structural analysis is the backbone of determining whether a beam, such as a wood beam in our exercise, can support the loads and moments it is subjected to. By assessing key variables like bending and shear stresses, engineers predict the behavior and strength of the beam.
Structural analysis involves:
  • Calculating moments and forces to understand stress distribution.
  • Determining section properties like modulus \( Z \) and first moment \( Q \).
  • Merging these calculations with material properties to ensure safety and functionality.
Ultimately, structural analysis provides a blueprint for making informed decisions about materials, safety margins, and design modifications, ensuring that all stress limits are within allowable ranges. By thoroughly understanding these principles, one can ensure that the design solution meets all necessary criteria.

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Most popular questions from this chapter

Because of foundation settlement, a circular tower is leaning at an angle \(\alpha\) to the vertical (see figure). The structural core of the tower is a circular cylinder of height \(h,\) outer diameter \(d_{2},\) and inner diameter \(d_{1} .\) For simplicity in the analysis, assume that the weight of the tower is uniformly distributed along the height. Obtain a formula for the maximum permissible angle \(\alpha\) if there is to be no tensile stress in the tower.

A square wood platform, \(2.4 \mathrm{m} \times 2.4 \mathrm{m}\) in area rests on masonry walls (see figure). The deck of the platform is constructed of \(50 \mathrm{mm}\) nominal thickness tongue-andgroove planks (actual thickness \(47 \mathrm{mm}\); see Appendix \(\mathrm{F}\) ) supported on two \(2.4-\mathrm{m}\) long beams. The beams have \(100 \mathrm{mm} \times 150 \mathrm{mm}\) nominal dimensions (actual dimensions \(97 \mathrm{mm} \times 147 \mathrm{mm}\) ). The planks are designed to support a uniformly distributed load \(w\left(\mathrm{kN} / \mathrm{m}^{2}\right)\) acting over the entire top surface of the platform. The allowable bending stress for the planks is \(17 \mathrm{MPa}\) and the allowable shear stress is 0.7 MPa. When analyzing the planks, disregard their weights and assume that their reactions are uniformly distributed over the top surfaces of the supporting beams. \(\begin{array}{lllll}\text { (a) } & \text { Determine } & \text { the } & \text { allowable } & \text { platform } & \text { load }\end{array}\) \(w_{1}\left(\mathrm{kN} / \mathrm{m}^{2}\right)\) based upon the bending stress in the planks. (b) Determine the allowable platform load \(w_{2}\left(\mathrm{kN} / \mathrm{m}^{2}\right)\) based upon the shear stress in the planks. (c) Which of the preceding values becomes the allowable load \(w_{\text {allow }}\) on the platform? (Hints: Use care in constructing the loading diagram for the planks, noting especially that the reactions are distributed loads instead of concentrated loads. Also, note that the maximum shear forces occur at the inside faces of the supporting beams.)

A so-called "trapeze bar" in a hospital room provides a means for paticnts to cxercise while in bed (sec figure). The bar is \(2.1 \mathrm{m}\) long and has a cross section in the shape of a regular octagon. The design load is \(1.2 \mathrm{kN}\) applied at the midpoint of the bar, and the allowable bending stress is \(200 \mathrm{MPa}\) Determine the minimum height \(h\) of the bar. (Assume that the ends of the bar are simply supported and that the weight of the bar is negligible.)

A cantilever beam \(A B\) with a rectangular cross section has a longitudinal hole drilled throughout its length (see figure). The beam supports a load \(P=600 \mathrm{N}\). The cross section is \(25 \mathrm{mm}\) wide and \(50 \mathrm{mm}\) high, and the hole has a diameter of \(10 \mathrm{mm}\) Find the bending stresses at the top of the beam, at the top of the hole, and at the bottom of the beam.

A small balcony constructed of wood is supported by three identical cantilever beams (see figure). Each beam has length \(L_{1}=2.1 \mathrm{m},\) width \(b,\) and height \(h=4 b / 3 .\) The dimensions of the balcony floor are \(L_{1} \times L_{2},\) with \(L_{2}=2.5 \mathrm{m} .\) The design load is \(5.5 \mathrm{kPa}\) acting over the entire floor area. (This load accounts for all loads except the weights of the cantilever beams, which have a weight density \(\gamma=5.5 \mathrm{kN} / \mathrm{m}^{3}\).) The allowable bending stress in the cantilevers is \(15 \mathrm{MPa}\) Assuming that the middle cantilever supports \(50 \%\) of the load and each outer cantilever supports \(25 \%\) of the load, determine the required dimensions \(b\) and \(h\)

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