Answer :
To solve this problem, we're going to use beam theory to determine the minimum required moment of inertia for the beam, ensuring that the vertical displacement of point A does not exceed 1/2 inch.
Assumptions and Given Data:
- The beam length from B to A is 5 ft and from A to C is 10 ft.
- The beam is subjected to a uniformly distributed load of 4 Kips/ft over the 5 ft span and a point load of 2 Kips point load at A.
- Modulus of Elasticity [tex]E = 29000 \text{ ksi}[/tex].
- Maximum allowable deflection at A [tex]\delta_{max} = \frac{1}{2} \text{ inch}[/tex].
Calculation Steps:
1. Determine Support Reactions:
Before applying the double integration method, you need to find the reactions at the supports.
Applying equilibrium equations:
Sum of moments about C:
[tex]5 \times 4 \times 5/2 + 2 \times 10 - R_B \times 15 = 0[/tex]
Simplify to find [tex]R_B[/tex]:
[tex]R_B = \frac{100 + 20}{15} = 8 \text{ Kips}[/tex]Sum of vertical forces:
[tex]R_B + R_C = 20 + 2[/tex]
[tex]R_C = 22 - 8 = 14 \text{ Kips}[/tex]
2. Use the Double Integration Method:
The elasticity and beam deflection relationship is given by:
[tex]EI \frac{d^2v}{dx^2} = M(x)[/tex]
Use known beam theory cases or integration to find the deflection at point A:
- Differential equation of the elastic curve is established using the moment equation.
- Integrate to find slope and deflection equations, using boundary conditions.
3. Calculate Moment of Inertia:
Given that [tex]\delta \leq \frac{1}{2} \text{ inch}[/tex].
Use the deflection equation that results from integrating the moment equation:
[tex]\frac{W L^3}{384 EI} + \frac{P a^2 b^2}{3 EI L} \leq \frac{1}{2} \text{ inch}[/tex]
4. Substitute Terms and Solve for
[tex]I[/tex]:
With calculated reactions and known loadings, solve the inequality:
[tex]I \geq \frac{L^3}{384 E} \left( \frac{1}{2} \text{ inch in converted units} \right)[/tex]
Ensure consistent units for calculations.
Conclusion:
By substituting the given values and solving this equation using the given modulus of elasticity, solve for the minimum moment of inertia [tex]I[/tex]. This ensures the deflection does not exceed the specified limit of 1/2 inch.
This process involves detailed application of static equilibrium and beam deflection theories, where accuracy in calculations and unit conversions is crucial.