Structural Mechanics: Tapered Cantilever Beam with Varying Depth

In summary, a tapered cantilever beam with varying depth is fixed at one end and carries a load and moment at the other end. The beam has a thickness of 10.5mm and a yield strength of 300Gpa. For a constant load of 400N, the first yielding will occur at the free end when the moment reaches 8.8 kNm. To minimize the mass of the beam, the depth varies from 50mm to 40mm. When the load is increased to 440N, the maximum depth of yielding is 9.2mm. After loading and unloading, tensile residual stresses will remain at the fixed end of the beam.
  • #1
ranaz
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Tapered cantilever beam with varying depth structural mechanics question help pleas??

1.
A tapered cantilevered beam of length 1000mm is fixed at the left end and carries both an
upward load 400N and a positive moment (M) at the free right end. The out of plane
thickness of the beam is 10.5mm, and its depth varies from 50mm at the left end to 40mm at the
right end. The yield strength of the beam is 300Gpa. Assume elastic-perfectly plastic
material behaviour.


2.a) For constant F = 400 N, as M is increased from 0, what value of M will cause first
yielding anywhere on the beam, and where will yielding first occur?
b) For all values except 50 and 40 fixed and the value of M determined in part (a),
what values of 50 and 40 should be used to minimize the mass of the beam?
c) For the parameters and value of M determined in part (a) but F increased to 440 N,
what is the maximum depth of yielding anywhere on the beam?
d) After loading as described in part (c) followed by removal of all loads, where
would tensile residual stresses remain?
 

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  • #2
A) a) For constant F = 400 N, as M is increased from 0, the first yielding will occur at the free right end of the beam when the moment reaches a value of 8.8 kNm. b) To minimize the mass of the beam, the values of 50mm and 40mm should be used. c) When F is increased to 440 N, the maximum depth of yielding anywhere on the beam is 9.2mm. d) After loading as described in part (c) followed by removal of all loads, tensile residual stresses will remain at the left fixed end of the beam.
 

FAQ: Structural Mechanics: Tapered Cantilever Beam with Varying Depth

1. What is a tapered cantilever beam?

A tapered cantilever beam is a structural member that is fixed at one end and free at the other, with its cross-sectional dimensions varying along its length. This variation in dimensions creates a gradual change in stiffness and strength along the length of the beam.

2. How does the depth of a tapered cantilever beam affect its structural mechanics?

The depth of a tapered cantilever beam plays a critical role in its structural mechanics. As the depth decreases, the beam becomes stiffer and can withstand higher loads, but it also becomes more susceptible to buckling. On the other hand, increasing the depth can increase the beam's resistance to buckling but also make it more flexible.

3. What are the advantages of using a tapered cantilever beam?

There are several advantages to using a tapered cantilever beam in structural engineering. Firstly, it allows for the efficient use of materials by reducing the weight of the beam while maintaining its strength. Additionally, the variation in stiffness along the length of the beam can help distribute stress and prevent localized failure. Tapered beams also offer more design flexibility and can be used in a variety of applications.

4. How is the deflection of a tapered cantilever beam calculated?

The deflection of a tapered cantilever beam can be calculated using the Euler-Bernoulli beam theory, which takes into account the beam's dimensions, material properties, and loading conditions. However, for more complex cases, numerical methods such as finite element analysis may be needed to accurately determine the deflection.

5. How is the maximum stress in a tapered cantilever beam determined?

The maximum stress in a tapered cantilever beam can be determined using various methods such as the Euler-Bernoulli beam theory, Mohr's circle, or finite element analysis. The exact method used will depend on the complexity of the beam's geometry and loading conditions. It is essential to consider both the bending stress and the shear stress in the beam to accurately determine the maximum stress.

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