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This is an excellent summary of the key pillars of Beam Theory, even for seasoned professionals, in a very concise delivery format, thank you Dr. Hernandez and hope that you continue distilling out similar content in the future!

About "c" that you are referring to in f(c), is it the location of the neutral axis in the strain diagram?

Hey, are these two deflection eqn found definitely right?

Theres a mistake in your integration at 3.42

En vaalkaiyai kaapathiviteergal aiyyaa

Thank you Dremph... Possibly the best explanation out there...no BS...just logic. Thanks

I am studying system identification and I found the 2 videos regarding state-space models of yours super helpful!!

THANK YOU

Interesting indeed!

Good presentation

If there were 3 legs, would all 3 be considered for torsional At/s?

If there were 3 legs, would all 3 be considered for torsional At/s?

Sir your videos are great....Sir i have a doubt that what is the purpose of using logarithm in calculation....?

Thanks a lot sir . The video is very informative . A small doubt sir. Like if we need to find the value of A i.e., cross sectional area ..., We can use the derived formula , but we also need to know the value of Integration constant. How to find it sir.

Great explanation.

❤

Weight

🤯

you are the best

Av including all legs or only the outers legs???

Thank you

can you share the code?

thank you very much

Not sure for shear. Critical Section is inclined, as shear stresses, in italian classical text, not vertical. Max Shear stress is at the centre of rectangular section, so your critical section should be at d/2 not at d. More you must consider that max shear stress at the centre is 1.5 times mean value. Where i wrong?

Thanks

This is what I was searching for..... amazing

Thank you sir,

Thank You Sir for Sharing!

How about if do moment in terms of y

Thank you so much. That was grate.

Thanks

you just saved my life.

great sir👍

Sir can you please make some videos on polar moment of inertia.

Can you name the text book?

Why is Torsion- Vu x e ??

Thank you for this!

Aoh should be equal to 174.25 in2 not 200.5 in2.

Hi! Thanks for the lecture :) I do have a question though, why is it @2:35 the Tt = 3.94 then @6:21 it became 4.55?

Awesome

1.Can you please tell that what if i takes a critical section for shear at the point of max. Shear force. Is the design wrong or it is only uneconomical but ok. 2.what should be the critical section if the beam is over hang from one side with 2 supports and a udl over the whole span.

Instead of providing only the corner bars can I provide reinforcing bars in the inner side as well? will that be able to resist the applied torsion?

Profesor que libro está usando?

Muy buen interpretación Eric.

Am I understanding it correctly that for the equation for determining transverse reinforcing you use the center line of that transverse reinforcement to determine area and for longitudinal reinforcement equation you use the outer edge of the transverse reinforcement to determine area?