Engineering Double overhanging beam deflection

AI Thread Summary
The discussion revolves around calculating the maximum slope and deflection of a double overhanging beam, with the original poster struggling for two weeks due to boundary and continuity conditions. They have established the shear force using a singularity function and integrated it to derive the moment equation. The conversation highlights the need to match integration constants with boundary conditions at specific points on the beam. Additionally, there is a caution regarding the reference points for evaluating slopes at supports, emphasizing the importance of correctly referencing variables in equations. The overall focus is on applying proper methods to achieve accurate results in beam deflection analysis.
Mohmmad Maaitah
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Homework Statement
Derive an expression for the slope and deflection for the beam
Relevant Equations
Deflection of beams
Please help me finding the max slope and deflection im stuck on this problem for two weeks.
I can't get anywhere with the boundry and continutiy conditions
The problem and what I've d one:
4585801D-87F3-45E4-888E-127D4A0C447C.jpg

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WhatsApp Image 2024-12-13 at 16.43.30_57b16c10.jpg

4585801D-87F3-45E4-888E-127D4A0C447C.jpg
 
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The shear ##V(x)## can be represented with the singularity function:

$$V(x) = -P+P\langle x - a \rangle^0 +P\langle x - (L-a) \rangle^0 $$

Then you can integrate that to get ##M(x)##

Then apply ## EI \frac{d^2y}{dx^2} = M(x) ##.

The boundary conditions on ##y## at ##x=a## and ##x = L-a## give you two equations and two unknowns to determine the integration constants ##C_\theta, C_y##
 
erobz said:
The shear ##V(x)## can be represented with the singularity function:

$$V(x) = -P+P\langle x - a \rangle^0 +P\langle x - (L-a) \rangle^0 $$

Then you can integrate that to get ##M(x)##

Then apply ## EI \frac{d^2y}{dx^2} = M(x) ##.

The boundary conditions on ##y## at ##x=a## and ##x = L-a## give you two equations and two unknowns to determine the integration constants ##C_\theta, C_y##
Thanks for the answer, how is it possible with the normal integration as I'm not familiar with the singularity method.
 
Mohmmad Maaitah said:
Thanks for the answer, how is it possible with the normal integration as I'm not familiar with the singularity method.
Its messy, but the idea is the same. You will have a bunch of integration constants to figure out. The is a distinct moment curve for each region of the beam between point loads with its own constants of integration in the deflection integration. They have to be all matched up with the boundary conditions on ##y## at a particular point and use the fact that we are not to have discontinuous slope between the segments.

I suggest you see this:

https://eng.libretexts.org/Bookshelves/Mechanical_Engineering/Introduction_to_Aerospace_Structures_and_Materials_(Alderliesten)/02:_Analysis_of_Statically_Determinate_Structures/07:_Deflection_of_Beams-_Geometric_Methods/7.04:_Deflection_by_Method_of_Singularity_Function
 
Mohmmad Maaitah said:
Homework Statement: Derive an expression for the slope and deflection for the beam
Relevant Equations: Deflection of beams

Please help me finding the max slope and deflection im stuck on this problem for two weeks.
I can't get anywhere with the boundry and continutiy conditions
The problem and what I've d one:
View attachment 354449
View attachment 354450View attachment 354451
View attachment 354449
I think you are going wrong in evaluating the slope at the first support. You apparently have ##x_2 = a ## in the equation? ##x_2## should not be referenced from the free end ( where ##x_1## is referenced), it should be referenced from the beginning of the segment under consideration. So when you are equating ##EI \theta_1 = EI \theta_2 ## be wary of that (pay attention to the value ##x_2## should take in the ##\theta_2## equation at the first support).
 
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