Vertical Deflection Off Free End Of Bar

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SUMMARY

The discussion focuses on calculating the vertical deflection of a cantilever beam with a point load. The user correctly calculated the shear stress using the formula Stress = F/A, resulting in 3,920,000 N/m². However, the user incorrectly applied the deflection formula, initially using ΔY = (F/A)(L/G), which is not suitable for this scenario. The correct formula for deflection at the free end of a cantilever beam is δ = FL³/(3EI), where F is the force, L is the length of the beam, E is Young's Modulus, and I is the moment of inertia.

PREREQUISITES
  • Understanding of shear stress calculations
  • Familiarity with Young's Modulus of materials
  • Knowledge of cantilever beam mechanics
  • Ability to apply formulas for beam deflection
NEXT STEPS
  • Research the formula for cantilever beam deflection: δ = FL³/(3EI)
  • Learn about the moment of inertia (I) for different cross-sectional shapes
  • Study Young's Modulus values for various materials
  • Explore practical applications of beam deflection in engineering
USEFUL FOR

Mechanical engineers, civil engineers, students studying structural mechanics, and anyone involved in beam design and analysis will benefit from this discussion.

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Homework Statement



The drawing shows a 152-kg crate hanging from the end of a steel bar. The length of the bar is 0.09 m, and its cross-sectional area is 3.80x10^-4 m^2. Neglect the weight of the bar itself.

(a) Determine the shear stress on the bar.
(b) Determine the vertical deflection ΔY of the right end of the bar.

Homework Equations


Stress=F/A
Tension=F=ma

Not quite sure what to do with deflection. I found ΔY=(F/A)(L/G) off another posts. Correct to use in this case?

The Attempt at a Solution



(a) This was pretty simple. Just found tension which was (152kg)(9.8). Then divided that by (3.8x10^-4). I got 3920000 N/m^2

(b) This is where I am having trouble. I used the equation off another problem.
This gave me ΔY=(3920000N/m^2)(.09m/(2.0x10^11)).
I found 2.0x10^11 by looking around for Young's Modulus of steel. This gave me an answer of 1.764x10^-6. However, the answer was marked wrong.

Help please!
 
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I assume you have a cantilever type of beam with a point load of 152 kg acting at the free end. In which case for this type of loading, the end deflection is given by

δ= FL3/3EI

Look up cantilever end deflection for definition of the terms.
 

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