Thanks sir 👍

Thanks a lot sir very useful video

From which textbook u explained, I mean terminologies are from which textbook?

what about the the segments whuch are not completely under teh strip but some of the portion is being covered ?

you did not tell about the value of zp provided

Ye Truck ka horn q dal diya hai😅

Thanks for explanation, very useful.

upar upaar bataya. detail me kuch nhi bataya 😢

184 kaha se Aiya Sir

Very well explained

Tooo good ❤❤❤

Sir please make videos on step by step mix designs according to FAA and ICAO

step jump kar kar ke sikha rahe ho

step 5 me Zprovided 348 kaha se aaya aur Z required 234 kaha se aaya

sir bht mistake hain calculation part me

Plzz give IS code page nos also

How you get 97.40 % please exapalin

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How tension and compression is developed.....

How to determine the diameter if load is given...

Nice explanation

Sir can u explain in shear strength formula what is the other area in th formula which u have considered as zero directly .

Fub is 5×100×0.6= 300 Sir

good and perfect!

Better than my professor thanks...

Good explanation my concept is very clear about this topic ❤❤

I believe we can calculate the load from the slabs S1 and S2 to the beam AB by getting the area of the two trapezoidal portions which is 2 Nos x 1/2 x (5+2) x 1.5 = 10.5 m2. We then multiplied the total area of 10.5 m2 x 8.75 kN/m2 and you get a total load of 91.875 kN to be carried by the beam AB. However using the UDL method (?) as you did we get a sum of 23.12 kN/m which when multipled by the length of the beam, we get a higher value of 115 kN. Further to this, we must add the Wall Loads to the beam, the self-weight of the Beam and then add the factor to be able to truely use this information in day to day job. Please go through that difference between the UDL and the area method. I have done this with another example, again the area method (which is nearer to Etabs calculation and result) has a lower value when doing the UDL.

Sorry I have only one liked buttom 🥹❤❤❤ thankyou thankyou so much keep itt

Thank you so much sir

P ki value

Very bad

Sir how to remember all the value

Tiada sarikata susa faham.🥴

Sir in step two for Design load you have denoted by (Pu) and in the last step you have denoted (Pu) as applied load . which is correct?

One of best video in DSS and this subtopic...

Excellent

Why √3

Extremely well explained

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thank you sir, the content is very informative.....

Thanks for the lecture. Are we adding all the numbers that fall within the rectangular shape?

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The number of bolts provided How to provide them gusette flange and angle 24 bolts OR Gusette flange and angle 12 bolts Angle and base plate 12 bolts How to provide base plate bolts

2.5 kb d t fu nominal bearing capacity Sir, thickness t When gusette plate is 16mm When Angle is 75×75×10 So, t=16mm or 10mm

Sir, thickness t When gusette plate is 16mm When Angle is 75×75×10 So, t=16mm or 10mm

great concept sir thankyou for explanation

Excellent video. I was struggling to find which plate thickness to choose. Thank you.

may i write after correction of elevation step "final runway length "

If d is not given how to find d Area of contact is given