Your videos have helped me far more than my lecturer and the notes; before seeing them I really struggled to grasp the concepts of bending and how to calculate moments, stresses etc, but now it's becoming much clearer. Thanks a lot.
very clear explanation, thanks! I would follow all the course if you could give titles with lesson number like #1 #2 #3....so that the order is clear :)
I have a question. If you get this "diagonal" linear distribution of sigmas (plot on the top left of the board) and you have an I-beam, what happens on the top of the web (right below the flanges). The area in the y-height is small, and it has lot of stress. Shouldn't the I-beams have something like a X (two opposite triangles) shape? thanks
Yeah those come under composite sections and at that point stress diagram changes i. e it doesn't show diagonal distribution like this one.. Look up bending stresses in composite sections buddy..
If it becomes a cantilever, then the tensile stress will be at the top and compression stress at bottom. In cantilever beams, the top most fiber experiences stretching while the bottom extreme fiber experiences the most compression.
Your videos have helped me far more than my lecturer and the notes; before seeing them I really struggled to grasp the concepts of bending and how to calculate moments, stresses etc, but now it's becoming much clearer. Thanks a lot.
Thank you so much, your explanation style is fifty times better than my lecturer!!, and I'm in a high ranked university
+Faisal Alshammary what uni r u at
I did a diploma on engineering under him before going to uni. I didn't know how spoilt I was to have a teacher like him.
faolan1686 what is his name ?
fantastic teaching! so clear. wish all my lecturers were this good. thank you much for sharing
very clear explanation, thanks! I would follow all the course if you could give titles with lesson number like #1 #2 #3....so that the order is clear :)
Excellent videos! Helping me a great deal in HSC Engineering Studies. Thank you!
Your videos are amazing! I super appreciate the fine work and the fact that you're willing to share such valuable knowledge. Thank you!
Great Teacher SIR
Jamani jamani 😭😭😭
Booyah, ndiyabulela 🇿🇦
God will bless you! thank you so much!
the denominator must be indirectly proportional to the stress but it isn't. Why?
Wow...
where can I find a book about this lesson and diagrams?
2:31 hahaha teacher is alien
nice teaching style,any lecture on macaulay's method
thank you lecturer u so help me
wonderful indeed. thank you
sir please make a video explaining Mohr's circle also sir
Can anyone tell me name of professor in this viedio
I have a question. If you get this "diagonal" linear distribution of sigmas (plot on the top left of the board) and you have an I-beam, what happens on the top of the web (right below the flanges). The area in the y-height is small, and it has lot of stress.
Shouldn't the I-beams have something like a X (two opposite triangles) shape? thanks
Yeah those come under composite sections and at that point stress diagram changes i. e it doesn't show diagonal distribution like this one.. Look up bending stresses in composite sections buddy..
wow..
Hi, I need all leson about welding conection from this teacher, please help me!
Thank you!!!
Pdf for this lecture
How come there is tensile stress at top in the U section?
Shouldn't the top have compressive stress?
If it becomes a cantilever, then the tensile stress will be at the top and compression stress at bottom. In cantilever beams, the top most fiber experiences stretching while the bottom extreme fiber experiences the most compression.
how to find I
Is there someone learn it just for fun like me?
No